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EX. US-1 Plane Frame with Steel Design

After one analysis, member selection is requested. Since member sizes change during the member selection, another analysis is done followed by final code checking to verify that the final sizes meet the requirements of the code based on the latest analysis results.

This problem is installed with the program by default to C:\Users\Public\Public Documents\STAAD.Pro CONNECT Edition\Samples\Sample Models\US\US-1 Plane Frame with Steel Design.STD when you install the program.

where:
  • L = 15 ft, H1 = 20 ft, H2 = 15 ft, and H3 = 9 ft
  • WLx = 0.6 k/ft, WLy = 1.0 k/ft, RL = 0.9 k/ft, LL = 1.2 k/ft, P1 = 35 kips, P2 = 15 kips
  • Members 1, 3, & 4 are a W14x90, Members 5, 6, & 7 are a W21x50, Member 2 is a W10x49, Members 8 through 13 are a W18x35. All other members comprising the truss are a L4x4x1/4

Actual input is shown in bold lettering followed by explanation.

   STAAD PLANE EXAMPLE PROBLEM NO. 1

Every input has to start with the term STAAD. The term PLANE signifies that the structure is a plane frame structure and the geometry is defined through X and Y axes.

   UNIT FT KIP

Defines the input units for the data that follows.

   JOINT COORDINATES
   1  0.  0. ; 2  30  0 ; 3  0  20  0  6  30  20  0 
   7  0  35 ; 8  30  35 ; 9  7.5  35 ; 10  22.5  35. 
   11  15  35 ; 12  5.  38. ; 13  25  38 
   14  10  41 ; 15  20  41 ; 16  15  44

Joint number followed by X and Y coordinates are provided above. Since this is a plane structure, the Z coordinates need not be provided.

Note: Semicolons (;) are used as line separators to allow for input of multiple sets of data on one line.
   MEMBER INCIDENCE
   1 1 3 ; 2 3 7 ; 3 2 6 ; 4 6 8 ; 5 3 4 
   6 4 5 ; 7 5 6 ; 8 7 12 ; 9 12 14
   10 14 16 ; 11 15 16 ; 12 13 15 ; 13 8 13
   14 9 12 ; 15 9 14 ; 16 11 14 ; 17 11 15 
   18 10 15 ; 19 10 13 ; 20 7 9
   21 9 11 ; 22 10 11 ; 23 8 10

Defines the members by the joints to which they are connected.

   MEMBER PROPERTY AMERICAN
   1  3  4 TABLE ST W14X90 ; 2  TA ST W10X49
   5  6  7 TA ST W21X50 ; 8  TO  13  TA ST W18X35
   14  TO  23 TA ST L40404

Member properties are from the British steel table. The term ST stands for standard single section.

   MEMB TRUSS
   14 TO 23

The above command defines that members 14 through 23 are of type truss. This means that these members can carry only axial tension/compression and no moments.

   MEMB RELEASE
   5 START MZ

Member 5 has local moment-z (MZ) released at the start joint. This means that the member cannot carry any moment-z (i.e., strong axis moment) at node 3.

   UNIT INCH
   DEFINE MATERIAL START
   ISOTROPIC STEEL
   E 29000
   POISSON 0.3
   DENSITY 0.000283
   ALPHA 6e-006
   DAMP 0.03
   TYPE STEEL
   STRENGTH FY 36 FU 58 RY 1.5 RT 1.2
   END DEFINE MATERIAL

The DEFINE MATERAL START initiates input for a material definition, which can later be assigned to all members. STAAD.Pro has several built-in material definitions, including the ISOTROPIC STEEL material used here. The length unit is changed from FEET to INCH to facilitate the input in familiar units.

   CONSTANTS
   BETA 90.0 MEMB 3 4
   MATERIAL STEEL ALL
   UNIT FT

The CONSTANT command initiates input for material constants or material definition references. The BETA command specifies that members 3 and 4 are rotated by 90 degrees around their own longitudinal axis. See G.4.3 Relationship Between Global and Local Coordinates for the definition of the beta angle.

   SUPPORT 
   1 FIXED ; 2 PINNED

A fixed support is located at joint 1 and a pinned support at joint 2.

   PRINT MEMBER INFORMATION LIST 1 5 14
   PRINT MEMBER PROPERTY LIST 1 2 5 8 14

The above PRINT commands are self-explanatory. The LIST option restricts the print output to the members listed.

   LOADING 1 DEAD AND LIVE LOAD

Load case 1 is initiated followed by a title.

   SELFWEIGHT Y -1.0

One of the components of load case 1 is the selfweight of the structure acting in the global Y direction with a factor of -1.0. Since global Y is vertically upward, the factor of -1.0 indicates that this load will act downwards.

   JOINT LOAD
   4  5  FY  -15. ; 11  FY  -35.

Load 1 contains joint loads also. FY indicates that the load is a force in the global Y direction.

   MEMB LOAD 
   8  TO  13 UNI Y  -0.9 ; 6  UNI GY  -1.2

Load 1 contains member loads also. GY indicates that the load is in the global Y direction while Y indicates local Y direction. The term UNI stands for uniformly distributed load. Loads are applied on members 6, and 8 to 13.

   CALCULATE RAYLEIGH FREQUENCY

The above command at the end of load case 1, is an instruction to perform a natural frequency calculation based on the Rayleigh method using the data in the above load case.

   LOADING  2 WIND FROM LEFT 
   MEMBER LOAD 
   1  2  UNI  GX  0.6 ; 8  TO  10  UNI Y  -1.

Load case 2 is initiated and contains several member loads.

   * 1/3 RD INCREASE IS ACCOMPLISHED BY 75% LOAD
   LOAD COMB 3 75 PERCENT DL LL WL 
   1 0.75 2 0.75

The above command identifies a combination load (case no. 3) with a title. The second line provides the load cases and their respective factors used for the load combination.

Note: Any line beginning with an asterisk (* character) is treated as a comment line.
   PERFORM ANALYSIS

This command instructs the program to proceed with the analysis.

   LOAD LIST 1 3

The above command activates load cases 1 and 3 only for the commands to follow. This also means that load case 2 will be made inactive.

   PRINT MEMBER FORCES
   PRINT SUPPORT REACTION

The above PRINT commands are self-explanatory. Also note that all the forces and reactions will be printed for load cases 1 and 3 only.

   PARAMETER 
   CODE AISC UNIFIED
   NSF  0.85  ALL
   BEAM 1.0 ALL
   KY  1.2  MEMB  3  4 
   RATIO  0.9  ALL 
   PROFILE W14 MEMB  1  3  4

The PARAMETER command is used to specify steel design parameters such as net section factor (NSF), effective length factor for bending about the minor axis (KY), etc. Information on these parameters can be obtained from the manual where the implementation of the code is explained. The BEAM parameter is specified to perform design at every 1/12th point along the member length, which is also the default. The RATIO parameter specifies that the ratio of actual loading over section capacity should not exceed 0.9.

   SELECT ALL

The above command instructs the program to select the most economic section for all the members based on the results of the analysis.

   GROUP MEMB 1 3 4
   GROUP MEMB 5 6 7
   GROUP MEMB 8 TO 13
   GROUP MEMB 14 TO 23

Although the program selects the most economical section for all members, it is not always practical to use many different sizes in one structure. Grouping is a procedure by which the cross section which has the largest value for the specified attribute, which in this case is the default and hence the AREA, from among the associated member list, is assigned to all members in the list. Hence, the cross sections for members 1, 3 and 4 are replaced with the one with the largest area from among the three.

   PERFORM ANALYSIS

As a result of the selection and grouping, the member sizes are no longer the same as the ones used in the original analysis. Hence, it is necessary to reanalyze the structure using the new properties to get new values of forces in the members.

   PARAMETER
   BEAM 1.0 ALL
   RATIO 1.0 ALL
   TRACK 1.0 ALL 

A new set of values are now provided for the above parameters. The actual load to member capacity RATIO has been redefined as 1.0. The TRACK parameter tells the program to print out the design results to the intermediate level of descriptively.

   CHECK CODE ALL

With the above command, the latest member sizes with the latest analysis results are checked to verify that they satisfy the CODE specifications.

   STEEL TAKE OFF

This command instructs the program to list the length and weight of all the different member sizes.

   FINISH

This command terminates the STAAD run.

Input File

STAAD PLANE EXAMPLE PROBLEM NO. 1
UNIT FT KIP
JOINT COORDINATES
1 0. 0. ; 2 30 0 ; 3 0 20 0 6 30 20 0
7 0 35 ; 8 30 35 ; 9 7.5 35 ; 10 22.5 35.
11 15 35 ; 12 5. 38. ; 13 25 38
14 10 41 ; 15 20 41 ; 16 15 44
MEMBER INCIDENCE
1 1 3 ; 2 3 7 ; 3 2 6 ; 4 6 8 ; 5 3 4
6 4 5 ; 7 5 6 ; 8 7 12 ; 9 12 14
10 14 16 ; 11 15 16 ; 12 13 15 ; 13 8 13
14 9 12 ; 15 9 14 ; 16 11 14 ; 17 11 15
18 10 15 ; 19 10 13 ; 20 7 9
21 9 11 ; 22 10 11 ; 23 8 10
MEMBER PROPERTY AMERICAN
1 3 4 TA ST W14X90 ; 2 TA ST W10X49
5 6 7 TA ST W21X50 ; 8 TO 13 TA ST W18X35
14 TO 23 TA ST L40404
*MEMB TRUSS
*14 TO 23
MEMB RELEASE
5 START MZ
14 to 23 start MPY 0.99 MPZ 0.99
14 to 23 end MPY 0.99 MPZ 0.99
UNIT INCH
DEFINE MATERIAL START
ISOTROPIC STEEL
E 29000
POISSON 0.3
DENSITY 283e-006
ALPHA 6e-006
DAMP 0.03
TYPE STEEL
STRENGTH FY 36 FU 58 RY 1.5 RT 1.2
END DEFINE MATERIAL
CONSTANTS
MATERIAL STEEL ALL
BETA 90.0 MEMB 3 4
UNIT FT
SUPPORT
1 FIXED ; 2 PINNED
PRINT MEMBER INFORMATION LIST 1 5 14
PRINT MEMBER PROPERTY LIST 1 2 5 8 14
LOADING 1 DEAD AND LIVE LOAD
SELFWEIGHT Y -1.0
JOINT LOAD
4 5 FY -15. ; 11 FY -35.
MEMB LOAD
8 TO 13 UNI Y -0.9 ; 6 UNI GY -1.2
CALCULATE RAYLEIGH FREQUENCY
LOADING 2  WIND FROM LEFT
MEMBER LOAD
1 2 UNI GX 0.6 ; 8 TO 10 UNI Y -1.
* 1/3 RD INCREASE IS ACCOMPLISHED BY 75% LOAD
LOAD COMB 3 75 PERCENT DL LL WL
1 0.75 2 0.75
PERFORM ANALYSIS
LOAD LIST 1 3
PRINT MEMBER FORCES
PRINT SUPPORT REACTION
PARAMETER
CODE AISC UNIFIED
NSF 0.85 ALL
BEAM 1.0 ALL
KY 1.2 MEMB 3 4
RATIO 0.9 ALL
PROFILE W14 MEMB 1 3 4
SELECT ALL
GROUP MEMB 1 3 4
GROUP MEMB 5 6 7
GROUP MEMB 8 TO 13
GROUP MEMB 14 TO 23
PERFORM ANALYSIS
PARAMETER
BEAM 1.0 ALL
RATIO 1.0 ALL
TRACK 1.0 ALL
CHECK CODE ALL
STEEL TAKE OFF
FINISH

STAAD Output File

                                                                  PAGE NO.    1
             ****************************************************        
             *                                                  *        
             *           STAAD.Pro CONNECT Edition              *        
             *           Version  22.04.00.**                   *        
             *           Proprietary Program of                 *        
             *           Bentley Systems, Inc.                  *        
             *           Date=    APR 21, 2020                  *        
             *           Time=    15:41:31                      *        
             *                                                  *        
             *  Licensed to: Bentley Systems Inc                *        
             ****************************************************        
     1. STAAD PLANE EXAMPLE PROBLEM NO. 1
INPUT FILE: US-1 Plane Frame with Steel Design.STD
     2. UNIT FT KIP
     3. JOINT COORDINATES
     4. 1 0. 0. ; 2 30 0 ; 3 0 20 0 6 30 20 0
     5. 7 0 35 ; 8 30 35 ; 9 7.5 35 ; 10 22.5 35.
     6. 11 15 35 ; 12 5. 38. ; 13 25 38
     7. 14 10 41 ; 15 20 41 ; 16 15 44
     8. MEMBER INCIDENCE
     9. 1 1 3 ; 2 3 7 ; 3 2 6 ; 4 6 8 ; 5 3 4
    10. 6 4 5 ; 7 5 6 ; 8 7 12 ; 9 12 14
    11. 10 14 16 ; 11 15 16 ; 12 13 15 ; 13 8 13
    12. 14 9 12 ; 15 9 14 ; 16 11 14 ; 17 11 15
    13. 18 10 15 ; 19 10 13 ; 20 7 9
    14. 21 9 11 ; 22 10 11 ; 23 8 10
    15. MEMBER PROPERTY AMERICAN
    16. 1 3 4 TA ST W14X90 ; 2 TA ST W10X49
    17. 5 6 7 TA ST W21X50 ; 8 TO 13 TA ST W18X35
    18. 14 TO 23 TA ST L40404
    19. *MEMB TRUSS
    20. *14 TO 23
    21. MEMB RELEASE
    22. 5 START MZ
    23. 14 TO 23 START MPY 0.99 MPZ 0.99
    24. 14 TO 23 END MPY 0.99 MPZ 0.99
    25. UNIT INCH
    26. DEFINE MATERIAL START
    27. ISOTROPIC STEEL
    28. E 29000
    29. POISSON 0.3
    30. DENSITY 283E-006
    31. ALPHA 6E-006
    32. DAMP 0.03
    33. TYPE STEEL
    34. STRENGTH FY 36 FU 58 RY 1.5 RT 1.2
    35. END DEFINE MATERIAL
    36. CONSTANTS
    37. MATERIAL STEEL ALL
    38. BETA 90.0 MEMB 3 4
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    2
    39. UNIT FT
    40. SUPPORT
    41. 1 FIXED ; 2 PINNED
    42. PRINT MEMBER INFORMATION LIST 1 5 14
  MEMBER   INFORMAT LIST     1        
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    3
   MEMBER INFORMATION
   ------------------
   MEMBER    START    END         LENGTH     BETA
             JOINT   JOINT        (FEET)     (DEG)     RELEASES
      1        1       3          20.000     0.00
      5        3       4          10.000     0.00    000001000000
     14        9      12           3.905     0.00    000011000011
   ************ END OF DATA FROM INTERNAL STORAGE ************
    43. PRINT MEMBER PROPERTY LIST 1 2 5 8 14
  MEMBER   PROPERTY LIST     1        
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    4
   MEMBER PROPERTIES. UNIT - INCH
   -----------------
   MEMB   PROFILE              AX/          IZ/          IY/        IX/  
                               AY           AZ           SZ         SY
     1  ST  W14X90            26.50       999.00       362.00        4.06
                               6.16        13.73       142.71       49.93
     2  ST  W10X49            14.40       272.00        93.40        1.39
                               3.40         7.47        54.40       18.68
     5  ST  W21X50            14.70       984.00        24.90        1.14
                               7.90         4.66        94.62        7.63
     8  ST  W18X35            10.30       510.00        15.30        0.51
                               5.31         3.40        57.63        5.10
    14  ST  L40404             1.93         1.18         4.90        0.04
                               0.67         0.67         0.76        1.73
   ************ END OF DATA FROM INTERNAL STORAGE ************
    44. LOADING 1 DEAD AND LIVE LOAD
    45. SELFWEIGHT Y -1.0
    46. JOINT LOAD
    47. 4 5 FY -15. ; 11 FY -35.
    48. MEMB LOAD
    49. 8 TO 13 UNI Y -0.9 ; 6 UNI GY -1.2
    50. CALCULATE RAYLEIGH FREQUENCY
    51. LOADING 2  WIND FROM LEFT
    52. MEMBER LOAD
    53. 1 2 UNI GX 0.6 ; 8 TO 10 UNI Y -1.
    54. * 1/3 RD INCREASE IS ACCOMPLISHED BY 75% LOAD
    55. LOAD COMB 3 75 PERCENT DL LL WL
    56. 1 0.75 2 0.75
    57. PERFORM ANALYSIS
            P R O B L E M   S T A T I S T I C S
            -----------------------------------
     NUMBER OF JOINTS         16  NUMBER OF MEMBERS      23
     NUMBER OF PLATES          0  NUMBER OF SOLIDS        0
     NUMBER OF SURFACES        0  NUMBER OF SUPPORTS      2
           Using 64-bit analysis engine.
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    5
           SOLVER USED IS THE IN-CORE ADVANCED MATH SOLVER
   TOTAL      PRIMARY LOAD CASES =     2, TOTAL DEGREES OF FREEDOM =      43
   TOTAL LOAD COMBINATION  CASES =     1  SO FAR.
   **********************************************************
   *                                                        *
   * RAYLEIGH FREQUENCY FOR LOADING     1 =    3.13858 CPS  *
   * MAX DEFLECTION =  1.21777 INCH GLO X,  AT JOINT     7  *
   *                                                        *
   **********************************************************
    58. LOAD LIST 1 3
    59. PRINT MEMBER FORCES
  MEMBER   FORCES                     
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    6
   MEMBER END FORCES    STRUCTURE TYPE = PLANE
   -----------------
   ALL UNITS ARE -- KIP  FEET     (LOCAL )
  MEMBER  LOAD  JT     AXIAL   SHEAR-Y  SHEAR-Z   TORSION     MOM-Y      MOM-Z
      1    1     1     54.05     -2.00     0.00      0.00      0.00     -61.74
                 3    -52.25      2.00     0.00      0.00      0.00      21.74
           3     1     40.71     18.99     0.00      0.00      0.00     247.88
                 3    -39.36     -9.99     0.00      0.00      0.00      41.97
      2    1     3     33.81     -5.48     0.00      0.00      0.00     -21.74
                 7    -33.07      5.48     0.00      0.00      0.00     -60.47
           3     3     28.90     -0.16     0.00      0.00      0.00     -41.97
                 7    -28.35      6.91     0.00      0.00      0.00     -11.09
      3    1     2     58.79      0.00    -2.00      0.00     -0.00       0.00
                 6    -56.99      0.00     2.00      0.00     40.00       0.00
           3     2     55.17      0.00    -3.51      0.00      0.00       0.00
                 6    -53.82      0.00     3.51      0.00     70.15       0.00
      4    1     6     31.94      0.00    -5.48      0.00     59.02       0.00
                 8    -30.59      0.00     5.48      0.00     23.19       0.00
           3     6     31.66      0.00   -13.66      0.00    105.29       0.00
                 8    -30.65      0.00    13.66      0.00     99.65       0.00
      5    1     3     -3.48     18.45     0.00      0.00      0.00       0.00
                 4      3.48    -17.95     0.00      0.00      0.00     181.98
           3     3    -10.16     10.46     0.00      0.00      0.00       0.00
                 4     10.16    -10.09     0.00      0.00      0.00     102.77
      6    1     4     -3.48      2.95     0.00      0.00      0.00    -181.98
                 5      3.48      9.55     0.00      0.00      0.00     148.97
           3     4    -10.16     -1.16     0.00      0.00      0.00    -102.77
                 5     10.16     10.53     0.00      0.00      0.00      44.29
      7    1     5     -3.48    -24.55     0.00      0.00      0.00    -148.97
                 6      3.48     25.05     0.00      0.00      0.00     -99.03
           3     5    -10.16    -21.78     0.00      0.00      0.00     -44.29
                 6     10.16     22.16     0.00      0.00      0.00    -175.43
      8    1     7     36.53     16.62     0.00      0.00      0.00      60.47
                12    -36.43    -11.20     0.00      0.00      0.00      20.64
           3     7     37.60     10.47     0.00      0.00      0.00      11.09
                12    -37.52     -2.03     0.00      0.00      0.00      25.36
      9    1    12     36.77      8.94     0.00      0.00      0.00     -20.63
                14    -36.66     -3.52     0.00      0.00      0.00      56.94
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    7
   MEMBER END FORCES    STRUCTURE TYPE = PLANE
   -----------------
   ALL UNITS ARE -- KIP  FEET     (LOCAL )
  MEMBER  LOAD  JT     AXIAL   SHEAR-Y  SHEAR-Z   TORSION     MOM-Y      MOM-Z
           3    12     36.66      7.58     0.00      0.00      0.00     -25.36
                14    -36.58      0.87     0.00      0.00      0.00      44.93
     10    1    14     41.85    -19.60     0.00      0.00      0.00     -56.95
                16    -41.74     25.02     0.00      0.00      0.00     -73.14
           3    14     34.32    -13.87     0.00      0.00      0.00     -44.93
                16    -34.24     22.31     0.00      0.00      0.00     -60.54
     11    1    15     41.83    -19.63     0.00      0.00      0.00     -57.16
                16    -41.72     25.06     0.00      0.00      0.00     -73.14
           3    15     35.88    -15.65     0.00      0.00      0.00     -42.57
                16    -35.80     19.72     0.00      0.00      0.00     -60.54
     12    1    13     40.08      7.85     0.00      0.00      0.00     -27.16
                15    -39.97     -2.43     0.00      0.00      0.00      57.15
           3    13     27.72      8.78     0.00      0.00      0.00      -3.23
                15    -27.64     -4.71     0.00      0.00      0.00      42.56
     13    1     8     40.49     11.35     0.00      0.00      0.00      23.19
                13    -40.39     -5.92     0.00      0.00      0.00      27.16
           3     8     26.74     19.68     0.00      0.00      0.00      99.65
                13    -26.66    -15.61     0.00      0.00      0.00       3.23
     14    1     9     -2.27      0.01     0.00      0.00      0.00       0.00
                12      2.29      0.01     0.00      0.00      0.00       0.00
           3     9      5.63      0.01     0.00      0.00      0.00       0.00
                12     -5.61      0.01     0.00      0.00      0.00       0.00
     15    1     9      1.82      0.01     0.00      0.00      0.00      -0.00
                14     -1.78      0.01     0.00      0.00      0.00       0.00
           3     9     -4.73      0.01     0.00      0.00      0.00      -0.00
                14      4.76      0.01     0.00      0.00      0.00       0.00
     16    1    11    -24.42      0.02     0.00      0.00      0.00      -0.00
                14     24.45      0.02     0.00      0.00      0.00      -0.00
           3    11    -10.26      0.01     0.00      0.00      0.00      -0.00
                14     10.29      0.01     0.00      0.00      0.00      -0.00
     17    1    11    -21.23      0.02     0.00      0.00      0.00      -0.00
                15     21.27      0.02     0.00      0.00      0.00      -0.00
           3    11    -23.97      0.01     0.00      0.00      0.00      -0.00
                15     24.00      0.01     0.00      0.00      0.00      -0.00
     18    1    10     -1.71      0.01     0.00      0.00      0.00      -0.00
                15      1.75      0.01     0.00      0.00      0.00       0.00
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    8
   MEMBER END FORCES    STRUCTURE TYPE = PLANE
   -----------------
   ALL UNITS ARE -- KIP  FEET     (LOCAL )
  MEMBER  LOAD  JT     AXIAL   SHEAR-Y  SHEAR-Z   TORSION     MOM-Y      MOM-Z
           3    10      5.69      0.01     0.00      0.00      0.00      -0.00
                15     -5.66      0.01     0.00      0.00      0.00       0.00
     19    1    10      1.97      0.01     0.00      0.00      0.00       0.00
                13     -1.95      0.01     0.00      0.00      0.00       0.00
           3    10     -6.90      0.01     0.00      0.00      0.00       0.00
                13      6.91      0.01     0.00      0.00      0.00       0.00
     20    1     7    -17.29      0.02     0.00      0.00      0.00       0.00
                 9     17.29      0.02     0.00      0.00      0.00       0.00
           3     7    -19.94      0.02     0.00      0.00      0.00      -0.00
                 9     19.94      0.02     0.00      0.00      0.00       0.00
     21    1     9    -19.44      0.02     0.00      0.00      0.00       0.00
                11     19.44      0.02     0.00      0.00      0.00       0.00
           3     9    -14.52      0.02     0.00      0.00      0.00       0.00
                11     14.52      0.02     0.00      0.00      0.00       0.00
     22    1    10    -21.48      0.02     0.00      0.00      0.00       0.00
                11     21.48      0.02     0.00      0.00      0.00       0.00
           3    10     -5.75      0.02     0.00      0.00      0.00       0.00
                11      5.75      0.02     0.00      0.00      0.00       0.00
     23    1     8    -23.40      0.02     0.00      0.00      0.00       0.00
                10     23.40      0.02     0.00      0.00      0.00       0.00
           3     8      0.86      0.02     0.00      0.00      0.00       0.00
                10     -0.86      0.02     0.00      0.00      0.00      -0.00
   ************** END OF LATEST ANALYSIS RESULT **************
    60. PRINT SUPPORT REACTION
  SUPPORT  REACTION                   
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    9
   SUPPORT REACTIONS -UNIT KIP  FEET    STRUCTURE TYPE = PLANE
   -----------------
 JOINT  LOAD   FORCE-X   FORCE-Y   FORCE-Z     MOM-X     MOM-Y     MOM Z
      1    1      2.00     54.05      0.00      0.00      0.00    -61.74
           3    -18.99     40.71      0.00      0.00      0.00    247.88
      2    1     -2.00     58.79      0.00      0.00      0.00      0.00
           3     -3.51     55.17      0.00      0.00      0.00      0.00
   ************** END OF LATEST ANALYSIS RESULT **************
    61. PARAMETER
    62. CODE AISC UNIFIED
    63. NSF 0.85 ALL
    64. BEAM 1.0 ALL
    65. KY 1.2 MEMB 3 4
    66. RATIO 0.9 ALL
    67. PROFILE W14 MEMB 1 3 4
    68. SELECT ALL
 PARAMETER 1       
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   10
                       STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.1)
                     ********************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 ***NOTE : AISC 360-16 Design Statement for STAAD.Pro.
 *** AXIS CONVENTION ***:
 ========================
 The capacity results and intermediate results in the report follow the notations
 and axes labels as defined in the AISC 360-16 code.
 The analysis results are reported in STAAD.Pro axis convention and the AISC 360:16
 design results are reported in AISC 360-16 code axis convention.
   AISC Spec.      STAAD.Pro      Description
  ------------    -----------     -------------
       X               Z          Axis typically parallel to the sections principal major axis.
       Y               Y          Axis typically parallel to the sections principal minor axis.
       Z               X          Longitudinal axis perpendicular to the cross section.
 SECTION FORCES AXIS MAPPING: -
   AISC Spec.      STAAD.Pro      Description
  ------------    -----------     -------------
       Pz              FX         Axial force.
       Vy              FY         Shear force along minor axis.
       Vx              FZ         Shear force along major axis.
       Tz              MX         Torsional moment.
       My              MY         Bending moment about minor axis.
       Mx              MZ         Bending moment about major axis.
 *** DESIGN MESSAGES ***:
 =======================
    1. Section classification reported is for the cross section and loadcase that
       produced the worst case design ratio for flexure/compression Capacity results.     
    2. Results for any Capacity/Check that is not relevant for a section/loadcase
       based on the code clause in AISC 360-16 will not be shown in the report.     
    3. Bending results are reported as being �about� the relevant axis (X/Y), while 
       the results for shear are reported as being for shear forces �along� the axis.
       E.g : Mx indicates bending about the X axis, while Vx indicates shear along
       the X axis.
 *** ABBREVIATIONS ***:
 ======================
    F-T-B = Flexural-Torsional Buckling
    L-T-B = Lateral-Torsional Buckling
    F-L-B = Flange Local Buckling
    W-L-B = Web Local Buckling
    L-L-B = Leg Local Buckling
    C-F-Y = Compression Flange Yielding
    T-F-Y = Tension Flange Yielding
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   11
                       STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.1)
                     ********************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     1 
|-----------------------------------------------------------------------------|
|  Member No:        1       Profile:  ST  W14X74              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.798       Loadcase:        3    |
|  Location:      0.00       Ref:      Cl.F2.2                                |
|  Pz:       40.71     C     Vy:        18.99           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      247.9        |
|-----------------------------------------------------------------------------|
 - Member :     2 
|-----------------------------------------------------------------------------|
|  Member No:        2       Profile:  ST  W12X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.726       Loadcase:        1    |
|  Location:     15.00       Ref:      Eq.H1-3b                               |
|  Pz:       33.07     C     Vy:       -5.481           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      60.47        |
|-----------------------------------------------------------------------------|
 - Member :     3 
|-----------------------------------------------------------------------------|
|  Member No:        3       Profile:  ST  W14X61              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.888       Loadcase:        3    |
|  Location:     20.00       Ref:      Eq.H1-1b                               |
|  Pz:       53.82     C     Vy:        0.000           Vx:     -3.507        |
|  Tz:       0.000           My:       -70.15           Mx:      0.000        |
|-----------------------------------------------------------------------------|
 - Member :     4 
|-----------------------------------------------------------------------------|
|  Member No:        4       Profile:  ST  W14X90              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.538       Loadcase:        3    |
|  Location:      0.00       Ref:      Eq.H1-1b                               |
|  Pz:       31.66     C     Vy:        0.000           Vx:     -13.66        |
|  Tz:       0.000           My:        105.3           Mx:      0.000        |
|-----------------------------------------------------------------------------|
 - Member :     5 
|-----------------------------------------------------------------------------|
|  Member No:        5       Profile:  ST  W21X44              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.851       Loadcase:        1    |
|  Location:     10.00       Ref:      Eq.H1-1b                               |
|  Pz:       3.481     T     Vy:        17.95           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -182.0        |
|-----------------------------------------------------------------------------|
 - Member :     6 
|-----------------------------------------------------------------------------|
|  Member No:        6       Profile:  ST  W21X44              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.867       Loadcase:        1    |
|  Location:      2.50       Ref:      Eq.H1-1b                               |
|  Pz:       3.481     T     Vy:       -.1761           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -185.4        |
|-----------------------------------------------------------------------------|
 - Member :     7 
|-----------------------------------------------------------------------------|
|  Member No:        7       Profile:  ST  W21X44              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.822       Loadcase:        3    |
|  Location:     10.00       Ref:      Eq.H1-1b                               |
|  Pz:       10.16     T     Vy:       -22.16           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      175.4        |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   12
                       STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.1)
                     ********************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     8 
|-----------------------------------------------------------------------------|
|  Member No:        8       Profile:  ST  W14X22              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.821       Loadcase:        1    |
|  Location:      0.00       Ref:      Eq.H1-3b                               |
|  Pz:       36.53     C     Vy:        16.62           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      60.47        |
|-----------------------------------------------------------------------------|
 - Member :     9 
|-----------------------------------------------------------------------------|
|  Member No:        9       Profile:  ST  W14X22              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.766       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3b                               |
|  Pz:       36.66     C     Vy:        3.515           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -56.94        |
|-----------------------------------------------------------------------------|
 - Member :    10 
|-----------------------------------------------------------------------------|
|  Member No:       10       Profile:  ST  W12X26              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.816       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       41.74     C     Vy:       -25.02           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      73.14        |
|-----------------------------------------------------------------------------|
 - Member :    11 
|-----------------------------------------------------------------------------|
|  Member No:       11       Profile:  ST  W12X26              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.816       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       41.72     C     Vy:       -25.06           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      73.14        |
|-----------------------------------------------------------------------------|
 - Member :    12 
|-----------------------------------------------------------------------------|
|  Member No:       12       Profile:  ST  W14X22              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.795       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3b                               |
|  Pz:       39.97     C     Vy:        2.432           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -57.15        |
|-----------------------------------------------------------------------------|
 - Member :    13 
|-----------------------------------------------------------------------------|
|  Member No:       13       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.829       Loadcase:        3    |
|  Location:      0.00       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       26.74     C     Vy:        19.68           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      99.65        |
|-----------------------------------------------------------------------------|
 - Member :    14 
|-----------------------------------------------------------------------------|
|  Member No:       14       Profile:  ST  L20202              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.768       Loadcase:        3    |
|  Location:      1.95       Ref:      Eq.H2-1                                |
|  Pz:       5.618     C     Vy:       -.2092E-03       Vx:     -.2092E-03    |
|  Tz:       0.000           My:       -.4549E-02       Mx:     0.4549E-02    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   13
                       STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.1)
                     ********************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    15 
|-----------------------------------------------------------------------------|
|  Member No:       15       Profile:  ST  L25253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.249       Loadcase:        1    |
|  Location:      3.25       Ref:      Eq.H2-1                                |
|  Pz:       1.804     C     Vy:       -.1251E-03       Vx:     -.1251E-03    |
|  Tz:       0.000           My:       -.9994E-02       Mx:     0.9994E-02    |
|-----------------------------------------------------------------------------|
 - Member :    16 
|-----------------------------------------------------------------------------|
|  Member No:       16       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.820       Loadcase:        1    |
|  Location:      3.91       Ref:      Eq.H2-1                                |
|  Pz:       24.43     T     Vy:       0.2114E-03       Vx:     0.2114E-03    |
|  Tz:       0.000           My:       -.2237E-01       Mx:     0.2237E-01    |
|-----------------------------------------------------------------------------|
 - Member :    17 
|-----------------------------------------------------------------------------|
|  Member No:       17       Profile:  ST  L20204              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.877       Loadcase:        3    |
|  Location:      3.91       Ref:      Eq.H2-1                                |
|  Pz:       23.99     T     Vy:       0.1653E-03       Vx:     0.1653E-03    |
|  Tz:       0.000           My:       -.1677E-01       Mx:     0.1677E-01    |
|-----------------------------------------------------------------------------|
 - Member :    18 
|-----------------------------------------------------------------------------|
|  Member No:       18       Profile:  ST  L25253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.743       Loadcase:        3    |
|  Location:      3.25       Ref:      Eq.H2-1                                |
|  Pz:       5.680     C     Vy:       -.7942E-04       Vx:     -.7942E-04    |
|  Tz:       0.000           My:       -.7397E-02       Mx:     0.7397E-02    |
|-----------------------------------------------------------------------------|
 - Member :    19 
|-----------------------------------------------------------------------------|
|  Member No:       19       Profile:  ST  L20202              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.804       Loadcase:        3    |
|  Location:      2.28       Ref:      Eq.H2-1                                |
|  Pz:       6.907     T     Vy:       0.4779E-03       Vx:     0.4779E-03    |
|  Tz:       0.000           My:       -.4374E-02       Mx:     0.4374E-02    |
|-----------------------------------------------------------------------------|
 - Member :    20 
|-----------------------------------------------------------------------------|
|  Member No:       20       Profile:  ST  L25253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.790       Loadcase:        3    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       19.94     T     Vy:       -.2987E-04       Vx:     -.2987E-04    |
|  Tz:       0.000           My:       -.2461E-01       Mx:     0.2461E-01    |
|-----------------------------------------------------------------------------|
 - Member :    21 
|-----------------------------------------------------------------------------|
|  Member No:       21       Profile:  ST  L25253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.785       Loadcase:        1    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       19.44     T     Vy:       -.1450E-03       Vx:     -.1450E-03    |
|  Tz:       0.000           My:       -.3268E-01       Mx:     0.3268E-01    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   14
                       STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.1)
                     ********************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    22 
|-----------------------------------------------------------------------------|
|  Member No:       22       Profile:  ST  L25253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.861       Loadcase:        1    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       21.48     T     Vy:       -.1182E-03       Vx:     -.1182E-03    |
|  Tz:       0.000           My:       -.3275E-01       Mx:     0.3275E-01    |
|-----------------------------------------------------------------------------|
 - Member :    23 
|-----------------------------------------------------------------------------|
|  Member No:       23       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.800       Loadcase:        1    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       23.40     T     Vy:       -.6927E-04       Vx:     -.6927E-04    |
|  Tz:       0.000           My:       -.3254E-01       Mx:     0.3254E-01    |
|-----------------------------------------------------------------------------|
    69. GROUP MEMB 1 3 4
   GROUPING BASED ON MEMBER      4  (ST  W14X90          ) LIST=      1....
    70. GROUP MEMB 5 6 7
   GROUPING BASED ON MEMBER      7  (ST  W21X44          ) LIST=      5....
    71. GROUP MEMB 8 TO 13
   GROUPING BASED ON MEMBER     13  (ST  W14X30          ) LIST=      8....
    72. GROUP MEMB 14 TO 23
   GROUPING BASED ON MEMBER     23  (ST  L30253          ) LIST=     14....
    73. PERFORM ANALYSIS
    ** ALL CASES BEING MADE ACTIVE BEFORE RE-ANALYSIS. **
   **********************************************************
   *                                                        *
   * RAYLEIGH FREQUENCY FOR LOADING     1 =    2.92702 CPS  *
   * MAX DEFLECTION =  1.49837 INCH GLO X,  AT JOINT     7  *
   *                                                        *
   **********************************************************
    74. PARAMETER
    75. BEAM 1.0 ALL
    76. RATIO 1.0 ALL
    77. TRACK 1.0 ALL
    78. CHECK CODE ALL
 PARAMETER 2       
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   15
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 ***NOTE : AISC 360-16 Design Statement for STAAD.Pro.
 *** AXIS CONVENTION ***:
 ========================
 The capacity results and intermediate results in the report follow the notations
 and axes labels as defined in the AISC 360-16 code.
 The analysis results are reported in STAAD.Pro axis convention and the AISC 360:16
 design results are reported in AISC 360-16 code axis convention.
   AISC Spec.      STAAD.Pro      Description
  ------------    -----------     -------------
       X               Z          Axis typically parallel to the sections principal major axis.
       Y               Y          Axis typically parallel to the sections principal minor axis.
       Z               X          Longitudinal axis perpendicular to the cross section.
 SECTION FORCES AXIS MAPPING: -
   AISC Spec.      STAAD.Pro      Description
  ------------    -----------     -------------
       Pz              FX         Axial force.
       Vy              FY         Shear force along minor axis.
       Vx              FZ         Shear force along major axis.
       Tz              MX         Torsional moment.
       My              MY         Bending moment about minor axis.
       Mx              MZ         Bending moment about major axis.
 *** DESIGN MESSAGES ***:
 =======================
    1. Section classification reported is for the cross section and loadcase that
       produced the worst case design ratio for flexure/compression Capacity results.     
    2. Results for any Capacity/Check that is not relevant for a section/loadcase
       based on the code clause in AISC 360-16 will not be shown in the report.     
    3. Bending results are reported as being �about� the relevant axis (X/Y), while 
       the results for shear are reported as being for shear forces �along� the axis.
       E.g : Mx indicates bending about the X axis, while Vx indicates shear along
       the X axis.
 *** ABBREVIATIONS ***:
 ======================
    F-T-B = Flexural-Torsional Buckling
    L-T-B = Lateral-Torsional Buckling
    F-L-B = Flange Local Buckling
    W-L-B = Web Local Buckling
    L-L-B = Leg Local Buckling
    C-F-Y = Compression Flange Yielding
    T-F-Y = Tension Flange Yielding
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   16
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     1 
|-----------------------------------------------------------------------------|
|  Member No:        1       Profile:  ST  W14X90              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.622       Loadcase:        3    |
|  Location:      0.00       Ref:      Cl.F2.2                                |
|  Pz:       40.44     C     Vy:        19.06           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      252.5        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     64.935                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.622(PASS)           |
|          Loc  :    0.00            Condition :    Cl.F2.2                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     0.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   2.650E+01     Axx :   2.059E+01     Ayy :   6.160E+00               |
| Ixx :   9.990E+02     Iyy :   3.620E+02     J   :   4.060E+00               |
| Sxx+:   1.427E+02     Sxx-:   1.427E+02     Zxx :   1.570E+02               |
| Syy+:   4.993E+01     Syy-:   4.993E+01     Zyy :   7.560E+01               |
| Cw  :   1.593E+04     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        20.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender      10.21       N/A      15.89     Table.4.1a.Case1     |
| Web   : NonSlender      28.59       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         10.21      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         28.59     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   17
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     1 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      858.6       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      858.6       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    53.20      792.2       0.067     Cl.E3           1    0.00 |
| Flex. Buck. Y    53.20      687.7       0.077     Cl.E3           1    0.00 |
| Flex. Tor. Buck  53.20      728.1       0.073     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      400.3       0.000     Cl.G1           1    0.00 |
| Shear Y          19.06      133.1       0.143     Cl.G1           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     252.5      423.9       0.596     Cl.F2.1         3    0.00 |
| Flex. Yld. Y     0.000      204.1       0.000     Cl.F6.1         1    0.00 |
| L-T-B Abt X      252.5      406.2       0.622     Cl.F2.2         3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.651     Eq.H1-1b             3    0.00                 |
| Cl.H13-IP          0.621     Eq.H1-3a(H1-1b)      3    0.00                 |
| Cl.H13-OP          0.473     Eq.H1-3b             3    0.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   18
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     2 
|-----------------------------------------------------------------------------|
|  Member No:        2       Profile:  ST  W12X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.824       Loadcase:        1    |
|  Location:     15.00       Ref:      Eq.H1-3b                               |
|  Pz:       32.83     C     Vy:       -6.421           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      67.78        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    118.446                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.824(PASS)           |
|          Loc  :   15.00            Condition :    Eq.H1-3b                  |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:    15.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.790E+00     Axx :   5.738E+00     Ayy :   3.198E+00               |
| Ixx :   2.380E+02     Iyy :   2.030E+01     J   :   4.570E-01               |
| Sxx+:   3.870E+01     Sxx-:   3.870E+01     Zxx :   4.310E+01               |
| Syy+:   6.227E+00     Syy-:   6.227E+00     Zyy :   9.560E+00               |
| Cw  :   2.079E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        15.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       7.41       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         43.92       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          7.41      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         43.92     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   19
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     2 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      284.8       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      284.8       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    33.27      267.0       0.125     Cl.E3           1    0.00 |
| Flex. Buck. Y    33.27      136.1       0.245     Cl.E3           1    0.00 |
| Flex. Tor. Buck  33.27      241.3       0.138     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      111.5       0.000     Cl.G1           1    0.00 |
| Shear Y          7.155      69.08       0.104     Cl.G1           3   15.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     67.78      116.4       0.582     Cl.F2.1         1   15.00 |
| Flex. Yld. Y     0.000      25.81       0.000     Cl.F6.1         1    0.00 |
| L-T-B Abt X      67.78      96.67       0.701     Cl.F2.2         1   15.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.864     Eq.H1-1a             1   15.00                 |
| Cl.H13-IP          0.644     Eq.H1-3a(H1-1b)      1   15.00                 |
| Cl.H13-OP          0.824     Eq.H1-3b             1   15.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   20
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     3 
|-----------------------------------------------------------------------------|
|  Member No:        3       Profile:  ST  W14X90              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.380       Loadcase:        3    |
|  Location:     20.00       Ref:      Eq.H1-1b                               |
|  Pz:       53.46     C     Vy:        0.000           Vx:     -3.441        |
|  Tz:       0.000           My:       -68.83           Mx:      0.000        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     77.922                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.380(PASS)           |
|          Loc  :   20.00            Condition :    Eq.H1-1b                  |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:    20.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   2.650E+01     Axx :   2.059E+01     Ayy :   6.160E+00               |
| Ixx :   9.990E+02     Iyy :   3.620E+02     J   :   4.060E+00               |
| Sxx+:   1.427E+02     Sxx-:   1.427E+02     Zxx :   1.570E+02               |
| Syy+:   4.993E+01     Syy-:   4.993E+01     Zyy :   7.560E+01               |
| Cw  :   1.593E+04     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        20.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.20  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender      10.21       N/A      15.89     Table.4.1a.Case1     |
| Web   : NonSlender      28.59       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         10.21      10.79     28.38     Table.4.1b.Case13    |
| Web   : Compact         28.59     ******    ******     Table.4.1.           |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   21
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     3 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      858.6       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      858.6       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    58.80      792.2       0.074     Cl.E3           1    0.00 |
| Flex. Buck. Y    58.80      623.7       0.094     Cl.E3           1    0.00 |
| Flex. Tor. Buck  58.80      728.1       0.081     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          3.441      400.3       0.009     Cl.G1           3    0.00 |
| Shear Y          0.000      133.1       0.000     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     0.000      423.9       0.000     Cl.F2.1         1    0.00 |
| Flex. Yld. Y     68.83      204.1       0.337     Cl.F6.1         3   20.00 |
| L-T-B Abt X      0.000      406.2       0.000     Cl.F2.2         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.380     Eq.H1-1b             3   20.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   22
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     4 
|-----------------------------------------------------------------------------|
|  Member No:        4       Profile:  ST  W14X90              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.563       Loadcase:        3    |
|  Location:      0.00       Ref:      Eq.H1-1b                               |
|  Pz:       31.24     C     Vy:        0.000           Vx:     -13.91        |
|  Tz:       0.000           My:        110.4           Mx:      0.000        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     58.442                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.563(PASS)           |
|          Loc  :    0.00            Condition :    Eq.H1-1b                  |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     0.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   2.650E+01     Axx :   2.059E+01     Ayy :   6.160E+00               |
| Ixx :   9.990E+02     Iyy :   3.620E+02     J   :   4.060E+00               |
| Sxx+:   1.427E+02     Sxx-:   1.427E+02     Zxx :   1.570E+02               |
| Syy+:   4.993E+01     Syy-:   4.993E+01     Zyy :   7.560E+01               |
| Cw  :   1.593E+04     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        15.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.20  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender      10.21       N/A      15.89     Table.4.1a.Case1     |
| Web   : NonSlender      28.59       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         10.21      10.79     28.38     Table.4.1b.Case13    |
| Web   : Compact         28.59     ******    ******     Table.4.1.           |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   23
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     4 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      858.6       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      858.6       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    31.80      820.6       0.039     Cl.E3           1    0.00 |
| Flex. Buck. Y    31.80      717.3       0.044     Cl.E3           1    0.00 |
| Flex. Tor. Buck  31.80      769.0       0.041     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          13.91      400.3       0.035     Cl.G1           3    0.00 |
| Shear Y          0.000      133.1       0.000     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     0.000      423.9       0.000     Cl.F2.1         1    0.00 |
| Flex. Yld. Y    -110.4      204.1       0.541     Cl.F6.1         3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.563     Eq.H1-1b             3    0.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   24
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     5 
|-----------------------------------------------------------------------------|
|  Member No:        5       Profile:  ST  W21X44              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.838       Loadcase:        1    |
|  Location:     10.00       Ref:      Eq.H1-1b                               |
|  Pz:       4.327     T     Vy:        17.68           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -179.1        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     95.097                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.838(PASS)           |
|          Loc  :   10.00            Condition :    Eq.H1-1b                  |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:    10.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.300E+01     Axx :   5.850E+00     Ayy :   7.245E+00               |
| Ixx :   8.430E+02     Iyy :   2.070E+01     J   :   7.700E-01               |
| Sxx+:   8.145E+01     Sxx-:   8.145E+01     Zxx :   9.540E+01               |
| Syy+:   6.369E+00     Syy-:   6.369E+00     Zyy :   1.020E+01               |
| Cw  :   2.549E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        10.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:   120.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       7.22       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         56.57       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:   120.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          7.22      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         56.57     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   25
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     5 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        10.46      421.2       0.025     Cl.D2           3    0.00 |
| Ten. Rupt.       10.46      421.2       0.025     Cl.D2           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      374.0       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      256.6       0.000     Cl.E3           1    0.00 |
| Flex. Tor. Buck  0.000      316.0       0.000     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      113.7       0.000     Cl.G1           1    0.00 |
| Shear Y          18.13      156.5       0.116     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X    -179.1      257.6       0.695     Cl.F2.1         1   10.00 |
| Flex. Yld. Y     0.000      27.52       0.000     Cl.F6.1         1    0.00 |
| L-T-B Abt X     -179.1      214.0       0.837     Cl.F2.2         1   10.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.838     Eq.H1-1b             1   10.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   26
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     6 
|-----------------------------------------------------------------------------|
|  Member No:        6       Profile:  ST  W21X44              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.851       Loadcase:        1    |
|  Location:      2.50       Ref:      Eq.H1-1b                               |
|  Pz:       4.327     T     Vy:       -.4256           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -181.9        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     95.097                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.851(PASS)           |
|          Loc  :    2.50            Condition :    Eq.H1-1b                  |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     2.50, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.300E+01     Axx :   5.850E+00     Ayy :   7.245E+00               |
| Ixx :   8.430E+02     Iyy :   2.070E+01     J   :   7.700E-01               |
| Sxx+:   8.145E+01     Sxx-:   8.145E+01     Zxx :   9.540E+01               |
| Syy+:   6.369E+00     Syy-:   6.369E+00     Zyy :   1.020E+01               |
| Cw  :   2.549E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        10.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:   120.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       7.22       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         56.57       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:   120.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          7.22      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         56.57     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   27
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     6 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        10.46      421.2       0.025     Cl.D2           3    0.00 |
| Ten. Rupt.       10.46      421.2       0.025     Cl.D2           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      374.0       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      256.6       0.000     Cl.E3           1    0.00 |
| Flex. Tor. Buck  0.000      316.0       0.000     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      113.7       0.000     Cl.G1           1    0.00 |
| Shear Y          10.64      156.5       0.068     Cl.G1           3   10.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X    -181.9      257.6       0.706     Cl.F2.1         1    2.50 |
| Flex. Yld. Y     0.000      27.52       0.000     Cl.F6.1         1    0.00 |
| L-T-B Abt X     -181.9      214.0       0.850     Cl.F2.2         1    2.50 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.851     Eq.H1-1b             1    2.50                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   28
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     7 
|-----------------------------------------------------------------------------|
|  Member No:        7       Profile:  ST  W21X44              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.840       Loadcase:        3    |
|  Location:     10.00       Ref:      Eq.H1-1b                               |
|  Pz:       10.46     T     Vy:       -22.22           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      179.2        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     95.097                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.840(PASS)           |
|          Loc  :   10.00            Condition :    Eq.H1-1b                  |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:    10.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.300E+01     Axx :   5.850E+00     Ayy :   7.245E+00               |
| Ixx :   8.430E+02     Iyy :   2.070E+01     J   :   7.700E-01               |
| Sxx+:   8.145E+01     Sxx-:   8.145E+01     Zxx :   9.540E+01               |
| Syy+:   6.369E+00     Syy-:   6.369E+00     Zyy :   1.020E+01               |
| Cw  :   2.549E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:        10.000                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:   120.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       7.22       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         56.57       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:   120.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          7.22      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         56.57     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   29
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     7 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        10.46      421.2       0.025     Cl.D2           3    0.00 |
| Ten. Rupt.       10.46      421.2       0.025     Cl.D2           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      374.0       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      256.6       0.000     Cl.E3           1    0.00 |
| Flex. Tor. Buck  0.000      316.0       0.000     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      113.7       0.000     Cl.G1           1    0.00 |
| Shear Y          25.20      156.5       0.161     Cl.G1           1   10.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     179.2      257.6       0.696     Cl.F2.1         3   10.00 |
| Flex. Yld. Y     0.000      27.52       0.000     Cl.F6.1         1    0.00 |
| L-T-B Abt X      179.2      214.0       0.838     Cl.F2.2         3   10.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.840     Eq.H1-1b             3   10.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   30
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     8 
|-----------------------------------------------------------------------------|
|  Member No:        8       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.594       Loadcase:        1    |
|  Location:      0.00       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       34.94     C     Vy:        17.30           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      67.77        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     47.018                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.594(PASS)           |
|          Loc  :    0.00            Condition :    Eq.H1-3a(H1-1b            |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     0.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.850E+00     Axx :   5.182E+00     Ayy :   3.726E+00               |
| Ixx :   2.910E+02     Iyy :   1.960E+01     J   :   3.800E-01               |
| Sxx+:   4.217E+01     Sxx-:   4.217E+01     Zxx :   4.730E+01               |
| Syy+:   5.825E+00     Syy-:   5.825E+00     Zyy :   8.990E+00               |
| Cw  :   1.141E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         5.831                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       8.74       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         48.26       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          8.74      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         48.26     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   31
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     8 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      286.7       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      286.7       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    36.43      274.6       0.133     Cl.E3           3    0.00 |
| Flex. Buck. Y    36.43      250.1       0.146     Cl.E3           3    0.00 |
| Flex. Tor. Buck  36.43      261.2       0.139     Cl.E4           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      100.7       0.000     Cl.G1           1    0.00 |
| Shear Y          17.30      80.48       0.215     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     67.77      127.7       0.531     Cl.F2.1         1    0.00 |
| Flex. Yld. Y     0.000      24.27       0.000     Cl.F6.1         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.601     Eq.H1-1b             1    0.00                 |
| Cl.H13-IP          0.594     Eq.H1-3a(H1-1b)      1    0.00                 |
| Cl.H13-OP          0.481     Eq.H1-3b             1    0.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   32
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :     9 
|-----------------------------------------------------------------------------|
|  Member No:        9       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.495       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       35.18     C     Vy:        3.755           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -55.01        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     47.018                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.495(PASS)           |
|          Loc  :    5.83            Condition :    Eq.H1-3a(H1-1b            |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     5.83, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.850E+00     Axx :   5.182E+00     Ayy :   3.726E+00               |
| Ixx :   2.910E+02     Iyy :   1.960E+01     J   :   3.800E-01               |
| Sxx+:   4.217E+01     Sxx-:   4.217E+01     Zxx :   4.730E+01               |
| Syy+:   5.825E+00     Syy-:   5.825E+00     Zyy :   8.990E+00               |
| Cw  :   1.141E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         5.831                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       8.74       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         48.26       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          8.74      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         48.26     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   33
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :     9 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      286.7       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      286.7       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    35.61      274.6       0.130     Cl.E3           3    0.00 |
| Flex. Buck. Y    35.61      250.1       0.142     Cl.E3           3    0.00 |
| Flex. Tor. Buck  35.61      261.2       0.136     Cl.E4           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      100.7       0.000     Cl.G1           1    0.00 |
| Shear Y          9.153      80.48       0.114     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X    -55.01      127.7       0.431     Cl.F2.1         1    5.83 |
| Flex. Yld. Y     0.000      24.27       0.000     Cl.F6.1         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.501     Eq.H1-1b             1    5.83                 |
| Cl.H13-IP          0.495     Eq.H1-3a(H1-1b)      1    5.83                 |
| Cl.H13-OP          0.387     Eq.H1-3b             1    5.83                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   34
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    10 
|-----------------------------------------------------------------------------|
|  Member No:       10       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.632       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       40.64     C     Vy:       -24.36           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      71.29        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     47.018                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.632(PASS)           |
|          Loc  :    5.83            Condition :    Eq.H1-3a(H1-1b            |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     5.83, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.850E+00     Axx :   5.182E+00     Ayy :   3.726E+00               |
| Ixx :   2.910E+02     Iyy :   1.960E+01     J   :   3.800E-01               |
| Sxx+:   4.217E+01     Sxx-:   4.217E+01     Zxx :   4.730E+01               |
| Syy+:   5.825E+00     Syy-:   5.825E+00     Zyy :   8.990E+00               |
| Cw  :   1.141E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         5.831                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       8.74       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         48.26       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          8.74      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         48.26     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   35
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    10 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      286.7       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      286.7       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    40.73      274.6       0.148     Cl.E3           1    0.00 |
| Flex. Buck. Y    40.73      250.1       0.163     Cl.E3           1    0.00 |
| Flex. Tor. Buck  40.73      261.2       0.156     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      100.7       0.000     Cl.G1           1    0.00 |
| Shear Y          24.36      80.48       0.303     Cl.G1           1    5.83 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     71.29      127.7       0.558     Cl.F2.1         1    5.83 |
| Flex. Yld. Y     0.000      24.27       0.000     Cl.F6.1         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.639     Eq.H1-1b             1    5.83                 |
| Cl.H13-IP          0.632     Eq.H1-3a(H1-1b)      1    5.83                 |
| Cl.H13-OP          0.542     Eq.H1-3b             1    5.83                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   36
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    11 
|-----------------------------------------------------------------------------|
|  Member No:       11       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.632       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       40.62     C     Vy:       -24.40           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      71.29        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     47.018                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.632(PASS)           |
|          Loc  :    5.83            Condition :    Eq.H1-3a(H1-1b            |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     5.83, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.850E+00     Axx :   5.182E+00     Ayy :   3.726E+00               |
| Ixx :   2.910E+02     Iyy :   1.960E+01     J   :   3.800E-01               |
| Sxx+:   4.217E+01     Sxx-:   4.217E+01     Zxx :   4.730E+01               |
| Syy+:   5.825E+00     Syy-:   5.825E+00     Zyy :   8.990E+00               |
| Cw  :   1.141E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         5.831                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       8.74       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         48.26       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          8.74      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         48.26     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   37
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    11 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      286.7       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      286.7       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    40.71      274.6       0.148     Cl.E3           1    0.00 |
| Flex. Buck. Y    40.71      250.1       0.163     Cl.E3           1    0.00 |
| Flex. Tor. Buck  40.71      261.2       0.156     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      100.7       0.000     Cl.G1           1    0.00 |
| Shear Y          24.40      80.48       0.303     Cl.G1           1    5.83 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     71.29      127.7       0.558     Cl.F2.1         1    5.83 |
| Flex. Yld. Y     0.000      24.27       0.000     Cl.F6.1         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.639     Eq.H1-1b             1    5.83                 |
| Cl.H13-IP          0.632     Eq.H1-3a(H1-1b)      1    5.83                 |
| Cl.H13-OP          0.542     Eq.H1-3b             1    5.83                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   38
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    12 
|-----------------------------------------------------------------------------|
|  Member No:       12       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.502       Loadcase:        1    |
|  Location:      5.83       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       38.28     C     Vy:        2.675           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:     -55.24        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     47.018                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.502(PASS)           |
|          Loc  :    5.83            Condition :    Eq.H1-3a(H1-1b            |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     5.83, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.850E+00     Axx :   5.182E+00     Ayy :   3.726E+00               |
| Ixx :   2.910E+02     Iyy :   1.960E+01     J   :   3.800E-01               |
| Sxx+:   4.217E+01     Sxx-:   4.217E+01     Zxx :   4.730E+01               |
| Syy+:   5.825E+00     Syy-:   5.825E+00     Zyy :   8.990E+00               |
| Cw  :   1.141E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         5.831                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       8.74       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         48.26       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          8.74      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         48.26     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   39
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    12 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      286.7       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      286.7       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    38.37      274.6       0.140     Cl.E3           1    0.00 |
| Flex. Buck. Y    38.37      250.1       0.153     Cl.E3           1    0.00 |
| Flex. Tor. Buck  38.37      261.2       0.147     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      100.7       0.000     Cl.G1           1    0.00 |
| Shear Y          8.835      80.48       0.110     Cl.G1           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X    -55.24      127.7       0.433     Cl.F2.1         1    5.83 |
| Flex. Yld. Y     0.000      24.27       0.000     Cl.F6.1         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.509     Eq.H1-1b             1    5.83                 |
| Cl.H13-IP          0.502     Eq.H1-3a(H1-1b)      1    5.83                 |
| Cl.H13-OP          0.405     Eq.H1-3b             1    5.83                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   40
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    13 
|-----------------------------------------------------------------------------|
|  Member No:       13       Profile:  ST  W14X30              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.818       Loadcase:        3    |
|  Location:      0.00       Ref:      Eq.H1-3a(H1-1b)                        |
|  Pz:       26.80     C     Vy:        19.16           Vx:      0.000        |
|  Tz:       0.000           My:        0.000           Mx:      98.18        |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     47.018                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.818(PASS)           |
|          Loc  :    0.00            Condition :    Eq.H1-3a(H1-1b            |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     0.00, PROPERTIES UNIT: IN  )                  |
| Ag  :   8.850E+00     Axx :   5.182E+00     Ayy :   3.726E+00               |
| Ixx :   2.910E+02     Iyy :   1.960E+01     J   :   3.800E-01               |
| Sxx+:   4.217E+01     Sxx-:   4.217E+01     Zxx :   4.730E+01               |
| Syy+:   5.825E+00     Syy-:   5.825E+00     Zyy :   8.990E+00               |
| Cw  :   1.141E+03     x0  :   0.000E+00     y0  :   0.000E+00               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         5.831                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: NonSlender       8.74       N/A      15.89     Table.4.1a.Case1     |
| Web   : Slender         48.26       N/A      42.29     Table.4.1a.Case5     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact          8.74      10.79     28.38     Table.4.1b.Case10    |
| Web   : Compact         48.26     106.72    161.78     Table.4.1b.Case15    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   41
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    13 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        0.000      286.7       0.000     Cl.D2           1    0.00 |
| Ten. Rupt.       0.000      286.7       0.000     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    38.64      274.6       0.141     Cl.E3           1    0.00 |
| Flex. Buck. Y    38.64      250.1       0.155     Cl.E3           1    0.00 |
| Flex. Tor. Buck  38.64      261.2       0.148     Cl.E4           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X          0.000      100.7       0.000     Cl.G1           1    0.00 |
| Shear Y          19.16      80.48       0.238     Cl.G1           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. X     98.18      127.7       0.769     Cl.F2.1         3    0.00 |
| Flex. Yld. Y     0.000      24.27       0.000     Cl.F6.1         1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H1          0.822     Eq.H1-1b             3    0.00                 |
| Cl.H13-IP          0.818     Eq.H1-3a(H1-1b)      3    0.00                 |
| Cl.H13-OP          0.746     Eq.H1-3b             3    0.00                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   42
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    14 
|-----------------------------------------------------------------------------|
|  Member No:       14       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.193       Loadcase:        3    |
|  Location:      1.95       Ref:      Eq.H2-1                                |
|  Pz:       4.890     C     Vy:       -.2903E-03       Vx:     -.3134E-03    |
|  Tz:       0.000           My:       -.2770E-02       Mx:     0.2566E-02    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     61.594                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.193(PASS)           |
|          Loc  :    1.95            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     1.95, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         3.905                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   43
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    14 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        2.784      32.40       0.086     Cl.D2           1    3.91 |
| Ten. Rupt.       2.784      32.40       0.086     Cl.D2           1    3.91 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    4.893      27.15       0.180     Cl.E3           3    0.00 |
| Flex. Buck. Y    4.893      25.55       0.192     Cl.E3           3    0.00 |
| Flex. Buck. U    4.893      27.15       0.180     Cl.E3           3    0.00 |
| Flex. Buck. V    4.893      25.55       0.192     Cl.E3           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.3605E-02  9.137       0.000     Cl.G1           1    0.00 |
| Shear Y         0.3340E-02  10.96       0.000     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    0.2891E-18  1.752       0.000     Cl.F10.1        1    1.63 |
| Flex. Yld. V    0.4971E-02  2.270       0.002     Cl.F10.1        1    2.28 |
| L-T-B Abt U     -.2891E-18  1.642       0.000     Cl.F10.2        1    2.60 |
| F-L-B Abt U     -.2891E-18  1.709       0.000     Cl.F10.3        1    2.60 |
| F-L-B Abt V     -.5835E-03  2.213       0.000     Cl.F10.3        1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.193     Eq.H2-1              3    1.95                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   44
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    15 
|-----------------------------------------------------------------------------|
|  Member No:       15       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.130       Loadcase:        3    |
|  Location:      3.79       Ref:      Eq.H2-1                                |
|  Pz:       4.106     T     Vy:       0.2042E-03       Vx:     0.2205E-03    |
|  Tz:       0.000           My:       -.4630E-02       Mx:     0.4288E-02    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    102.522                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.130(PASS)           |
|          Loc  :    3.79            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.79, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         6.500                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   45
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    15 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        4.112      32.40       0.127     Cl.D2           3    6.50 |
| Ten. Rupt.       4.112      32.40       0.127     Cl.D2           3    6.50 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    2.276      22.47       0.101     Cl.E3           1    0.00 |
| Flex. Buck. Y    2.276      18.63       0.122     Cl.E3           1    0.00 |
| Flex. Buck. U    2.276      22.47       0.101     Cl.E3           1    0.00 |
| Flex. Buck. V    2.276      18.63       0.122     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.3285E-02  9.137       0.000     Cl.G1           1    0.00 |
| Shear Y         0.3043E-02  10.96       0.000     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    -.5782E-18  1.752       0.000     Cl.F10.1        3    2.17 |
| Flex. Yld. V    0.7994E-02  2.270       0.004     Cl.F10.1        1    3.25 |
| L-T-B Abt U     -.5782E-18  1.499       0.000     Cl.F10.2        3    2.17 |
| F-L-B Abt U     -.5782E-18  1.709       0.000     Cl.F10.3        3    2.17 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.130     Eq.H2-1              3    3.79                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   46
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    16 
|-----------------------------------------------------------------------------|
|  Member No:       16       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.758       Loadcase:        1    |
|  Location:      3.91       Ref:      Eq.H2-1                                |
|  Pz:       24.33     T     Vy:       0.2674E-03       Vx:     0.2887E-03    |
|  Tz:       0.000           My:       -.1203E-01       Mx:     0.1114E-01    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    123.188                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.758(PASS)           |
|          Loc  :    3.91            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.91, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         7.810                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:    93.72)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:    93.72)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   47
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    16 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        24.34      32.40       0.751     Cl.D2           1    7.81 |
| Ten. Rupt.       24.34      32.40       0.751     Cl.D2           1    7.81 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      19.49       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      14.57       0.000     Cl.E3           1    0.00 |
| Flex. Buck. U    0.000      19.49       0.000     Cl.E3           1    0.00 |
| Flex. Buck. V    0.000      14.57       0.000     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.6517E-02  9.137       0.001     Cl.G1           1    7.81 |
| Shear Y         0.6037E-02  10.96       0.001     Cl.G1           1    7.81 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    -.1156E-17  1.752       0.000     Cl.F10.1        1    2.60 |
| Flex. Yld. V    0.1640E-01  2.270       0.007     Cl.F10.1        1    3.91 |
| L-T-B Abt U     -.1156E-17  1.437       0.000     Cl.F10.2        1    2.60 |
| F-L-B Abt U     -.1156E-17  1.709       0.000     Cl.F10.3        1    2.60 |
| F-L-B Abt V     -.1718E-02  2.213       0.001     Cl.F10.3        1    7.81 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.758     Eq.H2-1              1    3.91                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   48
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    17 
|-----------------------------------------------------------------------------|
|  Member No:       17       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.732       Loadcase:        3    |
|  Location:      3.91       Ref:      Eq.H2-1                                |
|  Pz:       23.54     T     Vy:       0.2111E-03       Vx:     0.2280E-03    |
|  Tz:       0.000           My:       -.8997E-02       Mx:     0.8334E-02    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    123.188                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.732(PASS)           |
|          Loc  :    3.91            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.91, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         7.810                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:    93.72)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:    93.72)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   49
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    17 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        23.55      32.40       0.727     Cl.D2           3    7.81 |
| Ten. Rupt.       23.55      32.40       0.727     Cl.D2           3    7.81 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      19.49       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      14.57       0.000     Cl.E3           1    0.00 |
| Flex. Buck. U    0.000      19.49       0.000     Cl.E3           1    0.00 |
| Flex. Buck. V    0.000      14.57       0.000     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.6530E-02  9.137       0.001     Cl.G1           1    7.81 |
| Shear Y         0.6049E-02  10.96       0.001     Cl.G1           1    7.81 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    0.1156E-17  1.752       0.000     Cl.F10.1        3    3.25 |
| Flex. Yld. V    0.1638E-01  2.270       0.007     Cl.F10.1        1    3.91 |
| L-T-B Abt U     -.1156E-17  1.437       0.000     Cl.F10.2        1    5.21 |
| F-L-B Abt U     -.1156E-17  1.709       0.000     Cl.F10.3        1    5.21 |
| F-L-B Abt V     -.1801E-02  2.213       0.001     Cl.F10.3        1    7.81 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.732     Eq.H2-1              3    3.91                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   50
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    18 
|-----------------------------------------------------------------------------|
|  Member No:       18       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.284       Loadcase:        3    |
|  Location:      3.25       Ref:      Eq.H2-1                                |
|  Pz:       5.245     C     Vy:       -.1002E-03       Vx:     -.1082E-03    |
|  Tz:       0.000           My:       -.4277E-02       Mx:     0.3962E-02    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    102.522                                    |
| Allowable Slenderness Ratio :    200.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.284(PASS)           |
|          Loc  :    3.25            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.25, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         6.500                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      3 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   51
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    18 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        1.041      32.40       0.032     Cl.D2           1    6.50 |
| Ten. Rupt.       1.041      32.40       0.032     Cl.D2           1    6.50 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    5.252      22.47       0.234     Cl.E3           3    0.00 |
| Flex. Buck. Y    5.252      18.63       0.282     Cl.E3           3    0.00 |
| Flex. Buck. U    5.252      22.47       0.234     Cl.E3           3    0.00 |
| Flex. Buck. V    5.252      18.63       0.282     Cl.E3           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.3297E-02  9.137       0.000     Cl.G1           1    0.00 |
| Shear Y         0.3054E-02  10.96       0.000     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    0.5782E-18  1.752       0.000     Cl.F10.1        1    2.17 |
| Flex. Yld. V    0.8144E-02  2.270       0.004     Cl.F10.1        1    3.25 |
| L-T-B Abt U     -.5782E-18  1.499       0.000     Cl.F10.2        1    3.25 |
| F-L-B Abt U     -.5782E-18  1.709       0.000     Cl.F10.3        1    3.25 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.284     Eq.H2-1              3    3.25                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   52
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    19 
|-----------------------------------------------------------------------------|
|  Member No:       19       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.197       Loadcase:        3    |
|  Location:      2.28       Ref:      Eq.H2-1                                |
|  Pz:       6.345     T     Vy:       0.2830E-04       Vx:     0.3055E-04    |
|  Tz:       0.000           My:       -.2627E-02       Mx:     0.2433E-02    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :     61.594                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.197(PASS)           |
|          Loc  :    2.28            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     2.28, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         3.905                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:     0.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   53
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    19 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        6.348      32.40       0.196     Cl.D2           3    3.91 |
| Ten. Rupt.       6.348      32.40       0.196     Cl.D2           3    3.91 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    1.187      27.15       0.044     Cl.E3           1    0.00 |
| Flex. Buck. Y    1.187      25.55       0.046     Cl.E3           1    0.00 |
| Flex. Buck. U    1.187      27.15       0.044     Cl.E3           1    0.00 |
| Flex. Buck. V    1.187      25.55       0.046     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.3569E-02  9.137       0.000     Cl.G1           1    0.00 |
| Shear Y         0.3306E-02  10.96       0.000     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    0.2891E-18  1.752       0.000     Cl.F10.1        1    1.30 |
| Flex. Yld. V    0.4975E-02  2.270       0.002     Cl.F10.1        1    2.28 |
| L-T-B Abt U     -.2891E-18  1.642       0.000     Cl.F10.2        1    1.63 |
| F-L-B Abt U     -.2891E-18  1.709       0.000     Cl.F10.3        1    1.63 |
| F-L-B Abt V     -.5547E-03  2.213       0.000     Cl.F10.3        3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.197     Eq.H2-1              3    2.28                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   54
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    20 
|-----------------------------------------------------------------------------|
|  Member No:       20       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.571       Loadcase:        3    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       18.24     T     Vy:       -.4450E-04       Vx:     -.4805E-04    |
|  Tz:       0.000           My:       -.1349E-01       Mx:     0.1249E-01    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    118.295                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      3             Ratio     :        0.571(PASS)           |
|          Loc  :    3.75            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.75, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         7.500                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   55
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    20 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        18.24      32.40       0.563     Cl.D2           3    0.00 |
| Ten. Rupt.       18.24      32.40       0.563     Cl.D2           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      20.27       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      15.51       0.000     Cl.E3           1    0.00 |
| Flex. Buck. U    0.000      20.27       0.000     Cl.E3           1    0.00 |
| Flex. Buck. V    0.000      15.51       0.000     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.9577E-02  9.137       0.001     Cl.G1           1    0.00 |
| Shear Y         0.8870E-02  10.96       0.001     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    -.2313E-17  1.752       0.000     Cl.F10.1        1    3.13 |
| Flex. Yld. V    0.2301E-01  2.270       0.010     Cl.F10.1        1    3.75 |
| L-T-B Abt U     -.2313E-17  1.451       0.000     Cl.F10.2        1    3.13 |
| F-L-B Abt U     -.2313E-17  1.709       0.000     Cl.F10.3        1    3.13 |
| F-L-B Abt V     -.2066E-02  2.213       0.001     Cl.F10.3        1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.571     Eq.H2-1              3    3.75                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   56
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    21 
|-----------------------------------------------------------------------------|
|  Member No:       21       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.544       Loadcase:        1    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       17.29     T     Vy:       -.1952E-03       Vx:     -.2108E-03    |
|  Tz:       0.000           My:       -.1787E-01       Mx:     0.1655E-01    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    118.295                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.544(PASS)           |
|          Loc  :    3.75            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.75, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         7.500                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   57
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    21 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        17.29      32.40       0.534     Cl.D2           1    0.00 |
| Ten. Rupt.       17.29      32.40       0.534     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      20.27       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      15.51       0.000     Cl.E3           1    0.00 |
| Flex. Buck. U    0.000      20.27       0.000     Cl.E3           1    0.00 |
| Flex. Buck. V    0.000      15.51       0.000     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.9554E-02  9.137       0.001     Cl.G1           1    0.00 |
| Shear Y         0.8849E-02  10.96       0.001     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    0.1156E-17  1.752       0.000     Cl.F10.1        1    1.88 |
| Flex. Yld. V    0.2435E-01  2.270       0.011     Cl.F10.1        1    3.75 |
| L-T-B Abt U     -.1156E-17  1.451       0.000     Cl.F10.2        3    3.13 |
| F-L-B Abt U     -.1156E-17  1.709       0.000     Cl.F10.3        3    3.13 |
| F-L-B Abt V     -.6014E-03  2.213       0.000     Cl.F10.3        1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.544     Eq.H2-1              1    3.75                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   58
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    22 
|-----------------------------------------------------------------------------|
|  Member No:       22       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.604       Loadcase:        1    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       19.23     T     Vy:       -.1599E-03       Vx:     -.1726E-03    |
|  Tz:       0.000           My:       -.1797E-01       Mx:     0.1664E-01    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    118.295                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.604(PASS)           |
|          Loc  :    3.75            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.75, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         7.500                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      1 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      1 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   59
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    22 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        19.23      32.40       0.594     Cl.D2           1    0.00 |
| Ten. Rupt.       19.23      32.40       0.594     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X    0.000      20.27       0.000     Cl.E3           1    0.00 |
| Flex. Buck. Y    0.000      15.51       0.000     Cl.E3           1    0.00 |
| Flex. Buck. U    0.000      20.27       0.000     Cl.E3           1    0.00 |
| Flex. Buck. V    0.000      15.51       0.000     Cl.E3           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.9516E-02  9.137       0.001     Cl.G1           1    0.00 |
| Shear Y         0.8814E-02  10.96       0.001     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    0.2313E-17  1.752       0.000     Cl.F10.1        1    3.13 |
| Flex. Yld. V    0.2449E-01  2.270       0.011     Cl.F10.1        1    3.75 |
| L-T-B Abt U     0.2313E-17  1.534       0.000     Cl.F10.2        1    3.13 |
| F-L-B Abt U     -.1156E-17  1.709       0.000     Cl.F10.3        3    3.75 |
| F-L-B Abt V     -.1036E-02  2.213       0.000     Cl.F10.3        3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.604     Eq.H2-1              1    3.75                 |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   60
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
 - Member :    23 
|-----------------------------------------------------------------------------|
|  Member No:       23       Profile:  ST  L30253              (AISC SECTIONS)|
|  Status:        PASS       Ratio:         0.640       Loadcase:        1    |
|  Location:      3.75       Ref:      Eq.H2-1                                |
|  Pz:       20.38     T     Vy:       -.9821E-04       Vx:     -.1060E-03    |
|  Tz:       0.000           My:       -.1759E-01       Mx:     0.1629E-01    |
|-----------------------------------------------------------------------------|
| SLENDERNESS                                                                 |
| Actual Slenderness Ratio    :    118.295                                    |
| Allowable Slenderness Ratio :    300.000            LOC  :     0.00         |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS                                                             |
| Critical L/C  :      1             Ratio     :        0.640(PASS)           |
|          Loc  :    3.75            Condition :    Eq.H2-1                   |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES  (LOC:     3.75, PROPERTIES UNIT: IN  )                  |
| Ag  :   1.000E+00     Axx :   4.700E-01     Ayy :   5.640E-01               |
| Ixx :   9.095E-01     Iyy :   5.788E-01     J   :   1.178E-02               |
| Sxx+:   5.634E-01     Sxx-:   5.604E-01     Zxx :   4.733E-01               |
| Syy+:   4.326E-01     Syy-:   5.093E-01     Zyy :   1.042E+00               |
| Cw  :   1.141E+03     x0  :   5.432E-01     y0  :   7.929E-01               |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES                                                         |
| Fyld:        5184.000              Fu:        8351.999                      |
|-----------------------------------------------------------------------------|
| Actual Member Length:         7.500                                         |
| Design Parameters                                            (Rolled)       |
| Kx:    1.00  Ky:    1.00  NSF:    0.85  SLF:    1.00  CSP:    1.00          |
|-----------------------------------------------------------------------------|
| COMPRESSION CLASSIFICATION (L/C:      3 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Slender         13.30       N/A      12.77     Table.4.1a.Case3     |
| Web   : Slender         15.96       N/A      12.77     Table.4.1a.Case3     |
|                                                                             |
| FLEXURE CLASSIFICATION     (L/C:      3 LOC:    90.00)                      |
|                            λ         λp        λr       CASE                |
| Flange: Compact         13.30      15.33     25.83     Table.4.1b.Case12    |
| Web   : NonCompact      15.96      15.33     25.83     Table.4.1b.Case12    |
|-----------------------------------------------------------------------------|
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   61
                       STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.1)
                     *****************************************************
 ALL UNITS ARE - KIP  FEET (UNLESS OTHERWISE Noted).
                                                       - Member :    23 Contd.
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL TENSION                            |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Ten. Yld.        20.38      32.40       0.629     Cl.D2           1    0.00 |
| Ten. Rupt.       20.38      32.40       0.629     Cl.D2           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL COMPRESSION                        |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Buck. X   0.7803      20.27       0.038     Cl.E3           3    0.00 |
| Flex. Buck. Y   0.7803      15.51       0.050     Cl.E3           3    0.00 |
| Flex. Buck. U   0.7803      20.27       0.038     Cl.E3           3    0.00 |
| Flex. Buck. V   0.7803      15.51       0.050     Cl.E3           3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR SHEAR                                    |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Shear X         0.9449E-02  9.137       0.001     Cl.G1           1    0.00 |
| Shear Y         0.8752E-02  10.96       0.001     Cl.G1           1    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR BENDING                                  |
|-----------------------------------------------------------------------------|
|                    DEMAND    CAPACITY   RATIO     REFERENCE     L/C    LOC  |
|                                                                             |
| Flex. Yld. U    -.1156E-17  1.752       0.000     Cl.F10.1        1    1.25 |
| Flex. Yld. V    0.2397E-01  2.270       0.011     Cl.F10.1        1    3.75 |
| L-T-B Abt U     -.1156E-17  1.451       0.000     Cl.F10.2        1    1.25 |
| F-L-B Abt U     -.1156E-17  1.709       0.000     Cl.F10.3        1    1.25 |
| F-L-B Abt V     -.3818E-02  2.213       0.002     Cl.F10.3        3    0.00 |
|-----------------------------------------------------------------------------|
|                         CHECKS FOR AXIAL BEND INTERACTION                   |
|-----------------------------------------------------------------------------|
|                                                                             |
|                    RATIO      CRITERIA          L/C    LOC                  |
| Clause H2          0.640     Eq.H2-1              1    3.75                 |
|-----------------------------------------------------------------------------|
    79. STEEL TAKE OFF
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   62
 STEEL TAKE OFF  
   STEEL TAKE-OFF
   --------------
      PROFILE                 LENGTH(FEET)      WEIGHT(KIP )
   ST  W14X90                      55.00             4.950
   ST  W12X30                      15.00             0.448
   ST  W21X44                      30.00             1.324
   ST  W14X30                      34.99             1.051
   ST  L30253                      66.43             0.226
                                          ----------------
                                    TOTAL =          7.999
   ************ END OF DATA FROM INTERNAL STORAGE ************
    80. FINISH
             *********** END OF THE STAAD.Pro RUN ***********         
               **** DATE= APR 21,2020   TIME= 15:41:34 ****
      EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   63
         ************************************************************
         *   For technical assistance on STAAD.Pro, please visit    *
         *   http://www.bentley.com/en/support/                     *
         *                                                          *
         *   Details about additional assistance from               *
         *   Bentley and Partners can be found at program menu      *
         *   Help->Technical Support                                *
         *                                                          *
         *      Copyright (c) 1997-2017 Bentley Systems, Inc.       *
         *                http://www.bentley.com                    *
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