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 2024\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. 1Every 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 KIPDefines 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 44Joint 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 10Defines 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 L40404Member properties are from the British steel table. The term ST stands for standard single section.
MEMB TRUSS
14 TO 23The 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 MZMember 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 MATERIALThe 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 FTThe 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 PINNEDA 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 14The above PRINT commands are self-explanatory. The LIST option restricts the print output to the members listed.
LOADING 1 DEAD AND LIVE LOADLoad case 1 is initiated followed by a title.
SELFWEIGHT Y -1.0One 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 -1.2Load 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 FREQUENCYThe 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 0.75The 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 ANALYSISThis command instructs the program to proceed with the analysis.
LOAD LIST 1 3The 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 REACTIONThe 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 4The 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 ALLThe 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 23Although 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 ANALYSISAs 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 ALLWith the above command, the latest member sizes with the latest analysis results are checked to verify that they satisfy the CODE specifications.
STEEL TAKE OFFThis command instructs the program to list the length and weight of all the different member sizes.
FINISHThis command terminates the STAAD run.
STAAD PLANE EXAMPLE PROBLEM NO. 1
START JOB INFORMATION
ENGINEER DATE 28-Apr-23
END JOB INFORMATION
***********************************************
* STAAD.Pro Generated Comment *
***********************************************
* 3 0 20 0 6 30 20 0
***********************************************
UNIT FEET KIP
JOINT COORDINATES
1 0 0 0; 2 30 0 0; 3 0 20 0; 4 10 20 0; 5 20 20 0; 6 30 20 0; 7 0 35 0;
8 30 35 0; 9 7.5 35 0; 10 22.5 35 0; 11 15 35 0; 12 5 38 0; 13 25 38 0;
14 10 41 0; 15 20 41 0; 16 15 44 0;
MEMBER INCIDENCES
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
2 TABLE ST W10X49
8 TO 13 TABLE ST W18X35
14 TO 23 TABLE ST L40404
UNIT FEET KIP
MEMBER PROPERTY 'US (AISC 2023).db3'
1 3 4 TABLE 'W' ST 'W14X90'
5 TO 7 TABLE 'W' TC 'W21X50' WP 1 TH 0.183
*MEMB TRUSS
*14 TO 23
UNIT FEET KIP
MEMBER 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 INCHES KIP
DEFINE MATERIAL START
ISOTROPIC STEEL
E 29000
POISSON 0.3
DENSITY 0.000283
ALPHA 6e-06
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 MEMB 3 4
UNIT FEET KIP
SUPPORTS
1 FIXED
2 PINNED
PRINT MEMBER INFORMATION LIST 1 5 14
PRINT MEMBER PROPERTIES LIST 1 2 5 8 14
LOAD 1 DEAD AND LIVE LOAD
SELFWEIGHT Y -1
JOINT LOAD
4 5 FY -15
11 FY -35
MEMBER LOAD
8 TO 13 UNI Y -0.9
6 UNI GY -1.2
CALCULATE RAYLEIGH FREQUENCY
LOAD 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 1
CODE AISC UNIFIED 2016
NSF 0.85 ALL
BEAM 1 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 TO 7
GROUP MEMB 8 TO 13
GROUP MEMB 14 TO 23
PERFORM ANALYSIS
PARAMETER 2
CODE AISC UNIFIED 2016
BEAM 1 ALL
RATIO 1 ALL
TRACK 1 ALL
CHECK CODE ALL
STEEL TAKE OFF ALL
FINISH
STAAD Output File
PAGE NO. 1
****************************************************
* *
* STAAD.Pro 2023 *
* Version 23.00.03.** *
* Proprietary Program of *
* Bentley Systems, Inc. *
* Date= JUL 4, 2024 *
* Time= 11:24:10 *
* *
* Licensed to: Bentley Systems Inc *
****************************************************
1. STAAD PLANE EXAMPLE PROBLEM NO. 1
INPUT FILE: D:\Documentation\STAAD.Pro\_Automated_Py\output\2024-07-04\SPro_Output_Input_Files\Sample .. .STD
2. START JOB INFORMATION
3. ENGINEER DATE 28-APR-23
4. END JOB INFORMATION
5. ***********************************************
6. * STAAD.PRO GENERATED COMMENT *
7. ***********************************************
8. * 3 0 20 0 6 30 20 0
9. ***********************************************
10. UNIT FEET KIP
11. JOINT COORDINATES
12. 1 0 0 0; 2 30 0 0; 3 0 20 0; 4 10 20 0; 5 20 20 0; 6 30 20 0; 7 0 35 0
13. 8 30 35 0; 9 7.5 35 0; 10 22.5 35 0; 11 15 35 0; 12 5 38 0; 13 25 38 0
14. 14 10 41 0; 15 20 41 0; 16 15 44 0
15. MEMBER INCIDENCES
16. 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
17. 10 14 16; 11 15 16; 12 13 15; 13 8 13; 14 9 12; 15 9 14; 16 11 14
18. 17 11 15; 18 10 15; 19 10 13; 20 7 9; 21 9 11; 22 10 11; 23 8 10
19. MEMBER PROPERTY AMERICAN
20. 2 TABLE ST W10X49
21. 8 TO 13 TABLE ST W18X35
22. 14 TO 23 TABLE ST L40404
23. UNIT FEET KIP
24. MEMBER PROPERTY 'US (AISC 2023).DB3'
25. 1 3 4 TABLE 'W' ST 'W14X90'
26. 5 TO 7 TABLE 'W' TC 'W21X50' WP 1 TH 0.183
27. *MEMB TRUSS
28. *14 TO 23
29. UNIT FEET KIP
30. MEMBER RELEASE
31. 5 START MZ
32. 14 TO 23 START MPY 0.99 MPZ 0.99
33. 14 TO 23 END MPY 0.99 MPZ 0.99
34. UNIT INCHES KIP
35. DEFINE MATERIAL START
36. ISOTROPIC STEEL
37. E 29000
38. POISSON 0.3
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 2
39. DENSITY 0.000283
40. ALPHA 6E-06
41. DAMP 0.03
42. TYPE STEEL
43. STRENGTH FY 36 FU 58 RY 1.5 RT 1.2
44. END DEFINE MATERIAL
45. CONSTANTS
46. MATERIAL STEEL ALL
47. BETA 90 MEMB 3 4
48. UNIT FEET KIP
49. SUPPORTS
50. 1 FIXED
51. 2 PINNED
52. 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 ************
53. PRINT MEMBER PROPERTIES LIST 1 2 5 8 14
MEMBER PROPERTI 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 4.10
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 TC W21X50 41.05 2242.09 341.22 43.46
8.74 22.25 126.10 56.87
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 ************
54. LOAD 1 DEAD AND LIVE LOAD
55. SELFWEIGHT Y -1
56. JOINT LOAD
57. 4 5 FY -15
58. 11 FY -35
59. MEMBER LOAD
60. 8 TO 13 UNI Y -0.9
61. 6 UNI GY -1.2
62. CALCULATE RAYLEIGH FREQUENCY
63. LOAD 2 WIND FROM LEFT
64. MEMBER LOAD
65. 1 2 UNI GX 0.6
66. 8 TO 10 UNI Y -1.
67. * 1/3 RD INCREASE IS ACCOMPLISHED BY 75% LOAD
68. LOAD COMB 3 75 PERCENT DL LL WL
69. 1 0.75 2 0.75
70. PERFORM ANALYSIS
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 5
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.
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 = 4.03683 CPS *
* MAX DEFLECTION = 0.85201 INCH GLO X, AT JOINT 7 *
* *
**********************************************************
71. LOAD LIST 1 3
72. 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 56.09 -1.08 0.00 0.00 0.00 -40.81
3 -54.29 1.08 0.00 0.00 0.00 19.14
3 1 41.62 18.88 0.00 0.00 0.00 244.98
3 -40.27 -9.88 0.00 0.00 0.00 42.55
2 1 3 33.33 -4.73 0.00 0.00 0.00 -19.14
7 -32.60 4.73 0.00 0.00 0.00 -51.82
3 3 28.96 -0.30 0.00 0.00 0.00 -42.55
7 -28.41 7.05 0.00 0.00 0.00 -12.51
3 1 2 59.43 0.00 -1.08 0.00 0.00 0.00
6 -57.63 0.00 1.08 0.00 21.67 0.00
3 2 56.27 0.00 -3.62 0.00 0.00 0.00
6 -54.92 0.00 3.62 0.00 72.48 0.00
4 1 6 32.41 0.00 -4.73 0.00 42.22 0.00
8 -31.06 0.00 4.73 0.00 28.75 0.00
3 6 31.59 0.00 -13.80 0.00 107.91 0.00
8 -30.58 0.00 13.80 0.00 99.02 0.00
5 1 3 -3.65 20.96 0.00 0.00 0.00 0.00
4 3.65 -19.57 0.00 0.00 0.00 202.65
3 3 -10.17 11.31 0.00 0.00 0.00 0.00
4 10.17 -10.26 0.00 0.00 0.00 107.83
6 1 4 -3.65 4.57 0.00 0.00 0.00 -202.65
5 3.65 8.83 0.00 0.00 0.00 181.35
3 4 -10.17 -0.99 0.00 0.00 0.00 -107.83
5 10.17 11.04 0.00 0.00 0.00 47.69
7 1 5 -3.65 -23.83 0.00 0.00 0.00 -181.35
6 3.65 25.22 0.00 0.00 0.00 -63.89
3 5 -10.17 -22.29 0.00 0.00 0.00 -47.69
6 10.17 23.33 0.00 0.00 0.00 -180.39
8 1 7 37.49 15.49 0.00 0.00 0.00 51.82
12 -37.39 -10.07 0.00 0.00 0.00 22.71
3 7 37.43 10.65 0.00 0.00 0.00 12.51
12 -37.35 -2.21 0.00 0.00 0.00 25.01
9 1 12 37.60 8.66 0.00 0.00 0.00 -22.71
14 -37.49 -3.24 0.00 0.00 0.00 57.38
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 36.51 7.62 0.00 0.00 0.00 -25.00
14 -36.43 0.82 0.00 0.00 0.00 44.83
10 1 14 42.01 -19.70 0.00 0.00 0.00 -57.39
16 -41.90 25.13 0.00 0.00 0.00 -73.31
3 14 34.28 -13.84 0.00 0.00 0.00 -44.83
16 -34.20 22.28 0.00 0.00 0.00 -60.48
11 1 15 41.99 -19.73 0.00 0.00 0.00 -57.52
16 -41.89 25.15 0.00 0.00 0.00 -73.31
3 15 35.83 -15.62 0.00 0.00 0.00 -42.48
16 -35.75 19.69 0.00 0.00 0.00 -60.48
12 1 13 39.64 7.99 0.00 0.00 0.00 -26.75
15 -39.54 -2.57 0.00 0.00 0.00 57.52
3 13 27.75 8.76 0.00 0.00 0.00 -3.23
15 -27.67 -4.70 0.00 0.00 0.00 42.48
13 1 8 39.94 12.23 0.00 0.00 0.00 28.75
13 -39.84 -6.81 0.00 0.00 0.00 26.75
3 8 26.79 19.57 0.00 0.00 0.00 99.02
13 -26.71 -15.50 0.00 0.00 0.00 3.23
14 1 9 -1.41 0.01 0.00 0.00 0.00 0.00
12 1.43 0.01 0.00 0.00 0.00 0.00
3 9 5.49 0.01 0.00 0.00 0.00 0.00
12 -5.47 0.01 0.00 0.00 0.00 0.00
15 1 9 1.11 0.01 0.00 0.00 0.00 -0.00
14 -1.07 0.01 0.00 0.00 0.00 0.00
3 9 -4.61 0.01 0.00 0.00 0.00 -0.00
14 4.64 0.01 0.00 0.00 0.00 0.00
16 1 11 -23.81 0.02 0.00 0.00 0.00 -0.00
14 23.85 0.02 0.00 0.00 0.00 -0.00
3 11 -10.35 0.01 0.00 0.00 0.00 -0.00
14 10.38 0.01 0.00 0.00 0.00 -0.00
17 1 11 -21.84 0.02 0.00 0.00 0.00 -0.00
15 21.88 0.02 0.00 0.00 0.00 -0.00
3 11 -23.89 0.01 0.00 0.00 0.00 -0.00
15 23.92 0.01 0.00 0.00 0.00 -0.00
18 1 10 -1.08 0.01 0.00 0.00 0.00 -0.00
15 1.12 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 5.62 0.01 0.00 0.00 0.00 -0.00
15 -5.59 0.01 0.00 0.00 0.00 0.00
19 1 10 1.22 0.01 0.00 0.00 0.00 0.00
13 -1.20 0.01 0.00 0.00 0.00 0.00
3 10 -6.80 0.01 0.00 0.00 0.00 0.00
13 6.82 0.01 0.00 0.00 0.00 0.00
20 1 7 -19.45 0.02 0.00 0.00 0.00 0.00
9 19.45 0.02 0.00 0.00 0.00 0.00
3 7 -19.57 0.02 0.00 0.00 0.00 -0.00
9 19.57 0.02 0.00 0.00 0.00 0.00
21 1 9 -20.77 0.02 0.00 0.00 0.00 0.00
11 20.77 0.02 0.00 0.00 0.00 0.00
3 9 -14.28 0.02 0.00 0.00 0.00 0.00
11 14.28 0.02 0.00 0.00 0.00 0.00
22 1 10 -22.03 0.02 0.00 0.00 0.00 0.00
11 22.03 0.02 0.00 0.00 0.00 0.00
3 10 -5.62 0.02 0.00 0.00 0.00 0.00
11 5.62 0.02 0.00 0.00 0.00 0.00
23 1 8 -23.23 0.02 0.00 0.00 0.00 0.00
10 23.23 0.02 0.00 0.00 0.00 0.00
3 8 0.90 0.02 0.00 0.00 0.00 0.00
10 -0.90 0.02 0.00 0.00 0.00 -0.00
************** END OF LATEST ANALYSIS RESULT **************
73. 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 1.08 56.09 0.00 0.00 0.00 -40.81
3 -18.88 41.62 0.00 0.00 0.00 244.98
2 1 -1.08 59.43 0.00 0.00 0.00 0.00
3 -3.62 56.27 0.00 0.00 0.00 0.00
************** END OF LATEST ANALYSIS RESULT **************
74. PARAMETER 1
75. CODE AISC UNIFIED 2016
76. NSF 0.85 ALL
77. BEAM 1 ALL
78. KY 1.2 MEMB 3 4
79. RATIO 0.9 ALL
80. PROFILE W14 MEMB 1 3 4
81. SELECT ALL
PARAMETER 1
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 10
STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.2)
********************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
*** ERROR: FOR MEMB NO. 1, MEMBER SELECT IS NOT SUPPORTED WITH STANDARD SECTION DATABASE.
*** ERROR: FOR MEMB NO. 3, MEMBER SELECT IS NOT SUPPORTED WITH STANDARD SECTION DATABASE.
*** ERROR: FOR MEMB NO. 4, MEMBER SELECT IS NOT SUPPORTED WITH STANDARD SECTION DATABASE.
*** ERROR: FOR MEMB NO. 5, MEMBER SELECT IS NOT SUPPORTED WITH STANDARD SECTION DATABASE.
*** ERROR: FOR MEMB NO. 6, MEMBER SELECT IS NOT SUPPORTED WITH STANDARD SECTION DATABASE.
*** ERROR: FOR MEMB NO. 7, MEMBER SELECT IS NOT SUPPORTED WITH STANDARD SECTION DATABASE.
***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/U Z Axis typically parallel to the sections principal major axis.
Y/V 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 (V1.2)
********************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 2
|-----------------------------------------------------------------------------|
| Member No: 2 Profile: ST W12X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.680 Loadcase: 1 |
| Location: 15.00 Ref: Eq.H1-3b |
| Pz: 32.60 C Vy: -4.731 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 51.82 |
|-----------------------------------------------------------------------------|
- Member : 8
|-----------------------------------------------------------------------------|
| Member No: 8 Profile: ST W10X22 (AISC SECTIONS)|
| Status: PASS Ratio: 0.844 Loadcase: 1 |
| Location: 0.00 Ref: Eq.H1-3b |
| Pz: 37.49 C Vy: 15.49 Vx: 0.000 |
| Tz: 0.000 My: 0.000 Mx: 51.82 |
|-----------------------------------------------------------------------------|
- Member : 9
|-----------------------------------------------------------------------------|
| Member No: 9 Profile: ST W14X22 (AISC SECTIONS)|
| Status: PASS Ratio: 0.797 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3b |
| Pz: 37.49 C Vy: 3.236 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: -57.38 |
|-----------------------------------------------------------------------------|
- Member : 10
|-----------------------------------------------------------------------------|
| Member No: 10 Profile: ST W12X26 (AISC SECTIONS)|
| Status: PASS Ratio: 0.817 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3a(H1-1b) |
| Pz: 41.90 C Vy: -25.13 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 73.31 |
|-----------------------------------------------------------------------------|
- Member : 11
|-----------------------------------------------------------------------------|
| Member No: 11 Profile: ST W12X26 (AISC SECTIONS)|
| Status: PASS Ratio: 0.817 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3a(H1-1b) |
| Pz: 41.89 C Vy: -25.15 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 73.31 |
|-----------------------------------------------------------------------------|
- Member : 12
|-----------------------------------------------------------------------------|
| Member No: 12 Profile: ST W14X22 (AISC SECTIONS)|
| Status: PASS Ratio: 0.816 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3b |
| Pz: 39.54 C Vy: 2.565 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: -57.52 |
|-----------------------------------------------------------------------------|
- Member : 13
|-----------------------------------------------------------------------------|
| Member No: 13 Profile: ST W14X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.823 Loadcase: 3 |
| Location: 0.00 Ref: Eq.H1-3a(H1-1b) |
| Pz: 26.79 C Vy: 19.57 Vx: 0.000 |
| Tz: 0.000 My: 0.000 Mx: 99.02 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 12
STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.2)
********************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 14
|-----------------------------------------------------------------------------|
| Member No: 14 Profile: ST L20203 (AISC SECTIONS)|
| Status: PASS Ratio: 0.844 Loadcase: 3 |
| Location: 1.95 Ref: Eq.H2-1 |
| Pz: 5.479 C Vy: -.2087E-03 Vx: -.2087E-03 |
| Tz: 0.000 My: -.4547E-02 Mx: 0.4547E-02 |
|-----------------------------------------------------------------------------|
- Member : 15
|-----------------------------------------------------------------------------|
| Member No: 15 Profile: ST L25253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.209 Loadcase: 1 |
| Location: 2.71 Ref: Eq.H2-1 |
| Pz: 1.092 C Vy: -.1093E-02 Vx: -.1093E-02 |
| Tz: 0.000 My: -.9685E-02 Mx: 0.9685E-02 |
|-----------------------------------------------------------------------------|
- Member : 16
|-----------------------------------------------------------------------------|
| Member No: 16 Profile: ST L20204 (AISC SECTIONS)|
| Status: PASS Ratio: 0.883 Loadcase: 1 |
| Location: 3.91 Ref: Eq.H2-1 |
| Pz: 23.83 T Vy: 0.2128E-03 Vx: 0.2128E-03 |
| Tz: 0.000 My: -.2237E-01 Mx: 0.2237E-01 |
|-----------------------------------------------------------------------------|
- Member : 17
|-----------------------------------------------------------------------------|
| Member No: 17 Profile: ST L20204 (AISC SECTIONS)|
| Status: PASS Ratio: 0.874 Loadcase: 3 |
| Location: 3.91 Ref: Eq.H2-1 |
| Pz: 23.90 T Vy: 0.1655E-03 Vx: 0.1655E-03 |
| Tz: 0.000 My: -.1676E-01 Mx: 0.1676E-01 |
|-----------------------------------------------------------------------------|
- Member : 18
|-----------------------------------------------------------------------------|
| Member No: 18 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.702 Loadcase: 3 |
| Location: 3.25 Ref: Eq.H2-1 |
| Pz: 5.601 C Vy: -.7931E-04 Vx: -.7931E-04 |
| Tz: 0.000 My: -.7397E-02 Mx: 0.7397E-02 |
|-----------------------------------------------------------------------------|
- Member : 19
|-----------------------------------------------------------------------------|
| Member No: 19 Profile: ST L20202 (AISC SECTIONS)|
| Status: PASS Ratio: 0.793 Loadcase: 3 |
| Location: 2.28 Ref: Eq.H2-1 |
| Pz: 6.813 T Vy: 0.4798E-03 Vx: 0.4798E-03 |
| Tz: 0.000 My: -.4371E-02 Mx: 0.4371E-02 |
|-----------------------------------------------------------------------------|
- Member : 20
|-----------------------------------------------------------------------------|
| Member No: 20 Profile: ST L25253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.784 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 19.45 T Vy: -.1438E-03 Vx: -.1438E-03 |
| Tz: 0.000 My: -.3215E-01 Mx: 0.3215E-01 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 13
STAAD.PRO MEMBER SELECTION - AISC 360-16 LRFD (V1.2)
********************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 21
|-----------------------------------------------------------------------------|
| Member No: 21 Profile: ST L25253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.835 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 20.77 T Vy: -.1385E-03 Vx: -.1385E-03 |
| Tz: 0.000 My: -.3270E-01 Mx: 0.3270E-01 |
|-----------------------------------------------------------------------------|
- Member : 22
|-----------------------------------------------------------------------------|
| Member No: 22 Profile: ST L25253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.882 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 22.03 T Vy: -.1219E-03 Vx: -.1219E-03 |
| Tz: 0.000 My: -.3274E-01 Mx: 0.3274E-01 |
|-----------------------------------------------------------------------------|
- Member : 23
|-----------------------------------------------------------------------------|
| Member No: 23 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.799 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 23.23 T Vy: -.8389E-04 Vx: -.8389E-04 |
| Tz: 0.000 My: -.3247E-01 Mx: 0.3247E-01 |
|-----------------------------------------------------------------------------|
82. GROUP MEMB 1 3 4
GROUPING BASED ON MEMBER 4 (ST W14X90 ) LIST= 1....
83. GROUP MEMB 5 TO 7
GROUPING BASED ON MEMBER 7 (TC W21X50 ) LIST= 5....
84. GROUP MEMB 8 TO 13
GROUPING BASED ON MEMBER 13 (ST W14X30 ) LIST= 8....
85. GROUP MEMB 14 TO 23
GROUPING BASED ON MEMBER 23 (ST L30253 ) LIST= 14....
86. PERFORM ANALYSIS
** ALL CASES BEING MADE ACTIVE BEFORE RE-ANALYSIS. **
**********************************************************
* *
* RAYLEIGH FREQUENCY FOR LOADING 1 = 3.73301 CPS *
* MAX DEFLECTION = 1.02646 INCH GLO X, AT JOINT 7 *
* *
**********************************************************
87. PARAMETER 2
88. CODE AISC UNIFIED 2016
89. BEAM 1 ALL
90. RATIO 1 ALL
91. TRACK 1 ALL
92. CHECK CODE ALL
PARAMETER 2
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 14
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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/U Z Axis typically parallel to the sections principal major axis.
Y/V 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. 15
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 1
|-----------------------------------------------------------------------------|
| Member No: 1 Profile: ST W14X90 (STANDARD SECTI|NS)
| Status: PASS Ratio: 0.611 Loadcase: 3 |
| Location: 0.00 Ref: Eq.H1-3a(H1-1b) |
| Pz: 41.36 C Vy: 18.87 Vx: 0.000 |
| Tz: 0.000 My: 0.000 Mx: 248.0 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 64.935 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.611(PASS) |
| Loc : 0.00 Condition : Eq.H1-3a(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 : 4.100E+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.B4.1a.Case1 |
| Web : NonSlender 28.59 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 10.21 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 28.59 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 16
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 55.50 792.2 0.070 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 55.50 687.7 0.081 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 55.50 728.6 0.076 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 18.87 133.1 0.142 Cl.G1 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X 248.0 423.9 0.585 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 248.0 406.3 0.610 Cl.F2.2 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.640 Eq.H1-1b 3 0.00 |
| CL.H13-IP 0.611 Eq.H1-3a(H1-1b) 3 0.00 |
| CL.H13-OP 0.461 Eq.H1-3b 3 0.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 17
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 2
|-----------------------------------------------------------------------------|
| Member No: 2 Profile: ST W12X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.780 Loadcase: 1 |
| Location: 15.00 Ref: Eq.H1-3b |
| Pz: 32.30 C Vy: -5.610 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 58.97 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 118.446 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.780(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 : 7.147E+02 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.B4.1a.Case1 |
| Web : NonSlender 41.62 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 7.41 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 41.62 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 18
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 32.75 267.4 0.122 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 32.75 136.1 0.241 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 32.75 202.5 0.162 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 7.313 69.08 0.106 Cl.G1 3 15.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X 58.97 116.4 0.507 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 58.97 87.73 0.672 Cl.F2.2 1 15.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.835 Eq.H1-1a 1 15.00 |
| CL.H13-IP 0.567 Eq.H1-3a(H1-1b) 1 15.00 |
| CL.H13-OP 0.780 Eq.H1-3b 1 15.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 19
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 3
|-----------------------------------------------------------------------------|
| Member No: 3 Profile: ST W14X90 (STANDARD SECTI|NS)
| Status: PASS Ratio: 0.400 Loadcase: 3 |
| Location: 20.00 Ref: Eq.H1-1b |
| Pz: 54.68 C Vy: -0.000 Vx: -3.631 |
| Tz: -0.000 My: -72.62 Mx: -0.000 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 77.922 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.400(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 : 4.100E+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.B4.1a.Case1 |
| Web : NonSlender 28.59 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 10.21 10.79 28.38 Table.B4.1b.Case13 |
| Web : Compact 28.59 ****** ****** Table.B4.1. |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 20
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 59.36 792.2 0.075 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 59.36 623.7 0.095 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 59.36 728.6 0.081 Cl.E4 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 3.631 400.3 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 72.62 204.1 0.356 Cl.F6.1 3 20.00 |
| L-T-B ABT X 0.000 406.3 0.000 Cl.F2.2 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.400 Eq.H1-1b 3 20.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 21
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 4
|-----------------------------------------------------------------------------|
| Member No: 4 Profile: ST W14X90 (STANDARD SECTI|NS)
| Status: PASS Ratio: 0.580 Loadcase: 3 |
| Location: 0.00 Ref: Eq.H1-1b |
| Pz: 31.14 C Vy: 0.000 Vx: -14.06 |
| Tz: 0.000 My: 114.0 Mx: 0.000 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 58.442 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.580(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 : 4.100E+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.B4.1a.Case1 |
| Web : NonSlender 28.59 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 10.21 10.79 28.38 Table.B4.1b.Case13 |
| Web : Compact 28.59 ****** ****** Table.B4.1. |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 22
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 32.33 820.6 0.039 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 32.33 717.3 0.045 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 32.33 769.2 0.042 Cl.E4 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 14.06 400.3 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 -114.0 204.1 0.558 Cl.F6.1 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.580 Eq.H1-1b 3 0.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 23
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 5
|-----------------------------------------------------------------------------|
| Member No: 5 Profile: TC W21X50 (STANDARD SECTI|NS)
| Status: PASS Ratio: 0.429 Loadcase: 1 |
| Location: 10.00 Ref: Eq.H1-1b |
| Pz: 4.648 T Vy: 19.56 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: -202.5 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 41.623 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.429(PASS) |
| Loc : 10.00 Condition : Eq.H1-1b |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES (LOC: 10.00, PROPERTIES UNIT: IN ) |
| Ag : 4.105E+01 Axx : 7.020E+00 Ayy : 7.904E+00 |
| Ixx : 2.242E+03 Iyy : 3.412E+02 J : 4.346E+01 |
| Sxx+: 4.327E+02 Sxx-: 1.259E+02 Zxx : 1.755E+02 |
| Syy+: 5.687E+01 Syy-: 5.687E+01 Zyy : 9.126E+01 |
| Cw : 5.489E+03 x0 : 0.000E+00 y0 : -3.160E+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 6.02 N/A 15.89 Table.B4.1a.Case1 |
| Web : Slender 51.89 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 120.00) |
| λ λp λr CASE |
| Flange: Compact 6.02 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 12.87 161.78 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 24
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 5 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 10.43 1330. 0.008 Cl.D2 3 0.00 |
| TEN. RUPT. 10.43 1330. 0.008 Cl.D2 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 0.000 1280. 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 0.000 1190. 0.000 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 0.000 1164. 0.000 Cl.E4 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.000 136.5 0.000 Cl.G1 1 0.00 |
| SHEAR Y 20.95 170.7 0.123 Cl.G1 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. Y -0.000 245.7 0.000 Cl.F6.1 1 0.00 |
| L-T-B ABT X -202.5 473.7 0.428 Cl.F4.2 1 10.00 |
| COM. FLA. YLD -202.5 473.7 0.428 Cl.F4.1 1 10.00 |
| TEN. FLA. YLD -202.5 473.7 0.428 Cl.F4.4 1 10.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.429 Eq.H1-1b 1 10.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 25
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 6
|-----------------------------------------------------------------------------|
| Member No: 6 Profile: TC W21X50 (STANDARD SECTI|NS)
| Status: PASS Ratio: 0.446 Loadcase: 1 |
| Location: 3.33 Ref: Eq.H1-1b |
| Pz: 4.648 T Vy: 0.9113E-01 Vx: 0.000 |
| Tz: 0.000 My: 0.000 Mx: -210.3 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 41.623 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.446(PASS) |
| Loc : 3.33 Condition : Eq.H1-1b |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES (LOC: 3.33, PROPERTIES UNIT: IN ) |
| Ag : 4.105E+01 Axx : 7.020E+00 Ayy : 7.904E+00 |
| Ixx : 2.242E+03 Iyy : 3.412E+02 J : 4.346E+01 |
| Sxx+: 4.327E+02 Sxx-: 1.259E+02 Zxx : 1.755E+02 |
| Syy+: 5.687E+01 Syy-: 5.687E+01 Zyy : 9.126E+01 |
| Cw : 5.489E+03 x0 : 0.000E+00 y0 : -3.160E+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 6.02 N/A 15.89 Table.B4.1a.Case1 |
| Web : Slender 51.89 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 120.00) |
| λ λp λr CASE |
| Flange: Compact 6.02 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 12.87 161.78 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 26
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 6 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 10.43 1330. 0.008 Cl.D2 3 0.00 |
| TEN. RUPT. 10.43 1330. 0.008 Cl.D2 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 0.000 1280. 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 0.000 1190. 0.000 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 0.000 1164. 0.000 Cl.E4 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.000 136.5 0.000 Cl.G1 1 0.00 |
| SHEAR Y 11.24 170.7 0.066 Cl.G1 3 10.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. Y -0.000 245.7 0.000 Cl.F6.1 1 0.00 |
| L-T-B ABT X -210.3 473.7 0.444 Cl.F4.2 1 3.33 |
| COM. FLA. YLD -210.3 473.7 0.444 Cl.F4.1 1 3.33 |
| TEN. FLA. YLD -210.3 473.7 0.444 Cl.F4.4 1 3.33 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.446 Eq.H1-1b 1 3.33 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 27
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 7
|-----------------------------------------------------------------------------|
| Member No: 7 Profile: TC W21X50 (STANDARD SECTI|NS)
| Status: PASS Ratio: 0.576 Loadcase: 3 |
| Location: 10.00 Ref: Eq.H1-1b |
| Pz: 10.43 T Vy: -23.54 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 186.6 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 41.623 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.576(PASS) |
| Loc : 10.00 Condition : Eq.H1-1b |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES (LOC: 10.00, PROPERTIES UNIT: IN ) |
| Ag : 4.105E+01 Axx : 7.020E+00 Ayy : 7.904E+00 |
| Ixx : 2.242E+03 Iyy : 3.412E+02 J : 4.346E+01 |
| Sxx+: 4.327E+02 Sxx-: 1.259E+02 Zxx : 1.755E+02 |
| Syy+: 5.687E+01 Syy-: 5.687E+01 Zyy : 9.126E+01 |
| Cw : 5.489E+03 x0 : 0.000E+00 y0 : -3.160E+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 6.02 N/A 15.89 Table.B4.1a.Case1 |
| Web : Slender 51.89 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 120.00) |
| λ λp λr CASE |
| Flange: Compact 6.02 10.79 28.38 Table.B4.1b.Case10 |
| Web : NonCompact 90.92 53.80 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 28
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 7 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 10.43 1330. 0.008 Cl.D2 3 0.00 |
| TEN. RUPT. 10.43 1330. 0.008 Cl.D2 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 0.000 1280. 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 0.000 1190. 0.000 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 0.000 1164. 0.000 Cl.E4 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.000 136.5 0.000 Cl.G1 1 0.00 |
| SHEAR Y 25.23 170.7 0.148 Cl.G1 1 10.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. Y -0.000 245.7 0.000 Cl.F6.1 1 0.00 |
| L-T-B ABT X 186.6 326.1 0.572 Cl.F4.2 3 10.00 |
| COM. FLA. YLD 186.6 339.8 0.549 Cl.F4.1 3 10.00 |
| TEN. FLA. YLD -181.1 473.7 0.382 Cl.F4.4 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H1 0.576 Eq.H1-1b 3 10.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 29
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 8
|-----------------------------------------------------------------------------|
| Member No: 8 Profile: ST W14X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.526 Loadcase: 1 |
| Location: 0.00 Ref: Eq.H1-3a(H1-1b) |
| Pz: 35.81 C Vy: 16.17 Vx: 0.000 |
| Tz: 0.000 My: 0.000 Mx: 58.97 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 47.018 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.526(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 : 8.800E+02 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.B4.1a.Case1 |
| Web : Slender 46.22 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 3 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 8.74 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 46.22 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 30
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 36.26 278.2 0.130 Cl.E3 3 0.00 |
| FLEX. BUCK. Y 36.26 253.2 0.143 Cl.E3 3 0.00 |
| FLEX. TOR. BUCK 36.26 260.4 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 16.17 80.48 0.201 Cl.G1 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X 58.97 127.7 0.462 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 0.532 Eq.H1-1b 1 0.00 |
| CL.H13-IP 0.526 Eq.H1-3a(H1-1b) 1 0.00 |
| CL.H13-OP 0.415 Eq.H1-3b 1 0.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 31
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 9
|-----------------------------------------------------------------------------|
| Member No: 9 Profile: ST W14X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.498 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3a(H1-1b) |
| Pz: 35.92 C Vy: 3.444 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: -55.39 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 47.018 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.498(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 : 8.800E+02 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.B4.1a.Case1 |
| Web : Slender 45.67 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 8.74 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 45.67 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 32
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 36.01 279.1 0.129 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 36.01 254.0 0.142 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 36.01 261.2 0.138 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 8.842 80.48 0.110 Cl.G1 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X -55.39 127.7 0.434 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 0.504 Eq.H1-1b 1 5.83 |
| CL.H13-IP 0.498 Eq.H1-3a(H1-1b) 1 5.83 |
| CL.H13-OP 0.390 Eq.H1-3b 1 5.83 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 33
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 10
|-----------------------------------------------------------------------------|
| Member No: 10 Profile: ST W14X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.631 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3a(H1-1b) |
| Pz: 40.72 C Vy: -24.42 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 71.25 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 47.018 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.631(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 : 8.800E+02 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.B4.1a.Case1 |
| Web : Slender 46.07 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 8.74 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 46.07 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 34
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 40.81 278.4 0.147 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 40.81 253.4 0.161 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 40.81 260.6 0.157 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 24.42 80.48 0.303 Cl.G1 1 5.83 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X 71.25 127.7 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 0.638 Eq.H1-1b 1 5.83 |
| CL.H13-IP 0.631 Eq.H1-3a(H1-1b) 1 5.83 |
| CL.H13-OP 0.539 Eq.H1-3b 1 5.83 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 35
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 11
|-----------------------------------------------------------------------------|
| Member No: 11 Profile: ST W14X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.631 Loadcase: 1 |
| Location: 5.83 Ref: Eq.H1-3a(H1-1b) |
| Pz: 40.71 C Vy: -24.44 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: 71.25 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 47.018 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.631(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 : 8.800E+02 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.B4.1a.Case1 |
| Web : Slender 46.07 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 8.74 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 46.07 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 36
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 40.80 278.4 0.147 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 40.80 253.4 0.161 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 40.80 260.6 0.157 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 24.44 80.48 0.304 Cl.G1 1 5.83 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X 71.25 127.7 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 0.638 Eq.H1-1b 1 5.83 |
| CL.H13-IP 0.631 Eq.H1-3a(H1-1b) 1 5.83 |
| CL.H13-OP 0.539 Eq.H1-3b 1 5.83 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 37
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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: 37.65 C Vy: 2.843 Vx: -0.000 |
| Tz: -0.000 My: -0.000 Mx: -55.52 |
|-----------------------------------------------------------------------------|
| COMPRESSION 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 : 8.800E+02 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.B4.1a.Case1 |
| Web : Slender 45.67 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 8.74 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 45.67 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 38
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 37.74 279.1 0.135 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 37.74 254.0 0.149 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 37.74 261.2 0.144 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 8.806 80.48 0.109 Cl.G1 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X -55.52 127.7 0.435 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 0.400 Eq.H1-3b 1 5.83 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 39
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 13
|-----------------------------------------------------------------------------|
| Member No: 13 Profile: ST W14X30 (AISC SECTIONS)|
| Status: PASS Ratio: 0.807 Loadcase: 3 |
| Location: 0.00 Ref: Eq.H1-3a(H1-1b) |
| Pz: 26.93 C Vy: 18.96 Vx: 0.000 |
| Tz: 0.000 My: 0.000 Mx: 96.95 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 47.018 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.807(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 : 8.800E+02 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.B4.1a.Case1 |
| Web : Slender 45.30 N/A 42.29 Table.B4.1a.Case5 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 8.74 10.79 28.38 Table.B4.1b.Case10 |
| Web : Compact 45.30 106.72 161.78 Table.B4.1b.Case15 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 40
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
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 37.87 279.8 0.135 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 37.87 254.5 0.149 Cl.E3 1 0.00 |
| FLEX. TOR. BUCK 37.87 261.8 0.145 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 18.96 80.48 0.236 Cl.G1 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. X 96.95 127.7 0.759 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 0.812 Eq.H1-1b 3 0.00 |
| CL.H13-IP 0.807 Eq.H1-3a(H1-1b) 3 0.00 |
| CL.H13-OP 0.729 Eq.H1-3b 3 0.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 41
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 14
|-----------------------------------------------------------------------------|
| Member No: 14 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.356 Loadcase: 3 |
| Location: 0.00 Ref: Eq.H2-1 |
| Pz: 4.739 C Vy: -.1880E-02 Vx: -.2736E-02 |
| Tz: 0.000 My: 0.8516E-04 Mx: -.5852E-04 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 89.945 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.356(PASS) |
| Loc : 0.00 Condition : Eq.H2-1 |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES (LOC: 0.00, 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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 3 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 42
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 14 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 1.950 32.40 0.060 Cl.D2 1 3.91 |
| TEN. RUPT. 1.950 32.40 0.060 Cl.D2 1 3.91 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 4.739 27.15 0.175 Cl.E3 3 0.00 |
| FLEX. BUCK. Y 4.739 25.55 0.186 Cl.E3 3 0.00 |
| FLEX. BUCK. U 4.739 27.88 0.170 Cl.E3 3 0.00 |
| FLEX. BUCK. V 4.739 21.10 0.225 Cl.E3 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.3673E-02 9.137 0.000 Cl.G1 1 0.00 |
| SHEAR Y 0.2524E-02 10.96 0.000 Cl.G1 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. U -.2891E-18 2.344 0.000 Cl.F10.1 3 1.30 |
| FLEX. YLD. V 0.4319E-02 1.064 0.004 Cl.F10.1 1 1.95 |
| L-T-B ABT U -.2891E-18 1.871 0.000 Cl.F10.2 3 1.30 |
| F-L-B ABT U -.2891E-18 2.286 0.000 Cl.F10.3 3 1.30 |
| F-L-B ABT V -.2394E-03 1.038 0.000 Cl.F10.3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.356 Eq.H2-1 3 0.00 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 43
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 15
|-----------------------------------------------------------------------------|
| Member No: 15 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.201 Loadcase: 1 |
| Location: 3.25 Ref: Eq.H2-1 |
| Pz: 1.572 C Vy: -.4006E-04 Vx: -.5830E-04 |
| Tz: 0.000 My: -.5927E-02 Mx: 0.4073E-02 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 149.712 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.201(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 44
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 15 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 3.984 32.40 0.123 Cl.D2 3 6.50 |
| TEN. RUPT. 3.984 32.40 0.123 Cl.D2 3 6.50 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 1.582 22.47 0.070 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 1.582 18.63 0.085 Cl.E3 1 0.00 |
| FLEX. BUCK. U 1.582 24.22 0.065 Cl.E3 1 0.00 |
| FLEX. BUCK. V 1.582 10.08 0.157 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.3557E-02 9.137 0.000 Cl.G1 1 0.00 |
| SHEAR Y 0.2444E-02 10.96 0.000 Cl.G1 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. U -.2891E-18 2.344 0.000 Cl.F10.1 1 1.08 |
| FLEX. YLD. V 0.7192E-02 1.064 0.007 Cl.F10.1 1 3.25 |
| L-T-B ABT U -.2891E-18 1.606 0.000 Cl.F10.2 1 1.08 |
| F-L-B ABT U -.2891E-18 2.286 0.000 Cl.F10.3 1 1.08 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.201 Eq.H2-1 1 3.25 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 45
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 16
|-----------------------------------------------------------------------------|
| Member No: 16 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.746 Loadcase: 1 |
| Location: 3.91 Ref: Eq.H2-1 |
| Pz: 23.66 T Vy: 0.6421E-04 Vx: 0.9343E-04 |
| Tz: 0.000 My: -.1351E-01 Mx: 0.9283E-02 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 179.891 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.746(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 93.72) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 46
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 16 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 23.67 32.40 0.730 Cl.D2 1 7.81 |
| TEN. RUPT. 23.67 32.40 0.730 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 21.94 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. V 0.000 6.981 0.000 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.7090E-02 9.137 0.001 Cl.G1 1 7.81 |
| SHEAR Y 0.4873E-02 10.96 0.000 Cl.G1 1 7.81 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. U 0.1156E-17 2.344 0.000 Cl.F10.1 1 1.95 |
| FLEX. YLD. V 0.1639E-01 1.064 0.015 Cl.F10.1 1 3.91 |
| L-T-B ABT U -.1156E-17 1.489 0.000 Cl.F10.2 1 3.91 |
| F-L-B ABT U -.1156E-17 2.286 0.000 Cl.F10.3 1 3.91 |
| F-L-B ABT V -.6305E-03 1.038 0.001 Cl.F10.3 1 7.81 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.746 Eq.H2-1 1 3.91 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 47
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 17
|-----------------------------------------------------------------------------|
| Member No: 17 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.734 Loadcase: 3 |
| Location: 3.91 Ref: Eq.H2-1 |
| Pz: 23.42 T Vy: 0.5076E-04 Vx: 0.7386E-04 |
| Tz: 0.000 My: -.1012E-01 Mx: 0.6956E-02 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 179.891 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.734(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 93.72) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 48
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 17 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 23.43 32.40 0.723 Cl.D2 3 7.81 |
| TEN. RUPT. 23.43 32.40 0.723 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 21.94 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. V 0.000 6.981 0.000 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.7093E-02 9.137 0.001 Cl.G1 1 7.81 |
| SHEAR Y 0.4874E-02 10.96 0.000 Cl.G1 1 7.81 |
|-----------------------------------------------------------------------------|
| CHECKS FOR BENDING |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. YLD. U -.1156E-17 2.344 0.000 Cl.F10.1 1 3.91 |
| FLEX. YLD. V 0.1639E-01 1.064 0.015 Cl.F10.1 1 3.91 |
| L-T-B ABT U -.1156E-17 1.489 0.000 Cl.F10.2 1 3.91 |
| F-L-B ABT U -.1156E-17 2.286 0.000 Cl.F10.3 1 3.91 |
| F-L-B ABT V -.6442E-03 1.038 0.001 Cl.F10.3 1 7.81 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.734 Eq.H2-1 3 3.91 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 49
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 18
|-----------------------------------------------------------------------------|
| Member No: 18 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.635 Loadcase: 3 |
| Location: 3.25 Ref: Eq.H2-1 |
| Pz: 5.107 C Vy: -.2479E-04 Vx: -.3607E-04 |
| Tz: 0.000 My: -.4398E-02 Mx: 0.3022E-02 |
|-----------------------------------------------------------------------------|
| COMPRESSION SLENDERNESS |
| Actual Slenderness Ratio : 149.712 |
| Allowable Slenderness Ratio : 200.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.635(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 3 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 50
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 18 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 0.2722 32.40 0.008 Cl.D2 1 6.50 |
| TEN. RUPT. 0.2722 32.40 0.008 Cl.D2 1 6.50 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 5.115 22.47 0.228 Cl.E3 3 0.00 |
| FLEX. BUCK. Y 5.115 18.63 0.275 Cl.E3 3 0.00 |
| FLEX. BUCK. U 5.115 24.22 0.211 Cl.E3 3 0.00 |
| FLEX. BUCK. V 5.115 10.08 0.507 Cl.E3 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.3559E-02 9.137 0.000 Cl.G1 1 0.00 |
| SHEAR Y 0.2446E-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 2.344 0.000 Cl.F10.1 1 3.25 |
| FLEX. YLD. V 0.7217E-02 1.064 0.007 Cl.F10.1 1 3.25 |
| L-T-B ABT U -.5782E-18 1.606 0.000 Cl.F10.2 1 3.25 |
| F-L-B ABT U -.5782E-18 2.286 0.000 Cl.F10.3 1 3.25 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.635 Eq.H2-1 3 3.25 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 51
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 19
|-----------------------------------------------------------------------------|
| Member No: 19 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.194 Loadcase: 3 |
| Location: 1.95 Ref: Eq.H2-1 |
| Pz: 6.179 T Vy: -.8679E-04 Vx: -.1263E-03 |
| Tz: 0.000 My: -.2629E-02 Mx: 0.1807E-02 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 89.945 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.194(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 0.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 52
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 19 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 6.183 32.40 0.191 Cl.D2 3 3.91 |
| TEN. RUPT. 6.183 32.40 0.191 Cl.D2 3 3.91 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 0.2635 27.15 0.010 Cl.E3 1 0.00 |
| FLEX. BUCK. Y 0.2635 25.55 0.010 Cl.E3 1 0.00 |
| FLEX. BUCK. U 0.2635 27.88 0.009 Cl.E3 1 0.00 |
| FLEX. BUCK. V 0.2635 21.10 0.012 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.3667E-02 9.137 0.000 Cl.G1 1 0.00 |
| SHEAR Y 0.2520E-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 2.344 0.000 Cl.F10.1 1 1.63 |
| FLEX. YLD. V 0.4323E-02 1.064 0.004 Cl.F10.1 1 1.95 |
| L-T-B ABT U -.2891E-18 1.871 0.000 Cl.F10.2 3 1.63 |
| F-L-B ABT U -.2891E-18 2.286 0.000 Cl.F10.3 3 1.63 |
| F-L-B ABT V -.2196E-03 1.038 0.000 Cl.F10.3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.194 Eq.H2-1 3 1.95 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 53
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 20
|-----------------------------------------------------------------------------|
| Member No: 20 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.567 Loadcase: 3 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 17.84 T Vy: -.1479E-04 Vx: -.2153E-04 |
| Tz: 0.000 My: -.1474E-01 Mx: 0.1013E-01 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 172.745 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 3 Ratio : 0.567(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 90.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 54
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 20 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 17.84 32.40 0.550 Cl.D2 3 0.00 |
| TEN. RUPT. 17.84 32.40 0.550 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 22.50 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. V 0.000 7.571 0.000 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.1057E-01 9.137 0.001 Cl.G1 1 0.00 |
| SHEAR Y 0.7263E-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 2.344 0.000 Cl.F10.1 1 1.25 |
| FLEX. YLD. V 0.2350E-01 1.064 0.022 Cl.F10.1 1 3.75 |
| L-T-B ABT U -.1156E-17 1.516 0.000 Cl.F10.2 3 5.00 |
| F-L-B ABT U -.1156E-17 2.286 0.000 Cl.F10.3 3 5.00 |
| F-L-B ABT V -.7131E-03 1.038 0.001 Cl.F10.3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.567 Eq.H2-1 3 3.75 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 55
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 21
|-----------------------------------------------------------------------------|
| Member No: 21 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.597 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 18.63 T Vy: -.4916E-04 Vx: -.7154E-04 |
| Tz: 0.000 My: -.1965E-01 Mx: 0.1351E-01 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 172.745 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.597(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 90.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 56
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 21 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 18.63 32.40 0.575 Cl.D2 1 0.00 |
| TEN. RUPT. 18.63 32.40 0.575 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 22.50 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. V 0.000 7.571 0.000 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.1057E-01 9.137 0.001 Cl.G1 1 0.00 |
| SHEAR Y 0.7262E-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 2.344 0.000 Cl.F10.1 1 1.25 |
| FLEX. YLD. V 0.2385E-01 1.064 0.022 Cl.F10.1 1 3.75 |
| L-T-B ABT U -.1156E-17 1.516 0.000 Cl.F10.2 3 1.88 |
| F-L-B ABT U -.1156E-17 2.286 0.000 Cl.F10.3 3 1.88 |
| F-L-B ABT V -.3550E-03 1.038 0.000 Cl.F10.3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.597 Eq.H2-1 1 3.75 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 57
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 22
|-----------------------------------------------------------------------------|
| Member No: 22 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.631 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 19.71 T Vy: -.4426E-04 Vx: -.6440E-04 |
| Tz: 0.000 My: -.1967E-01 Mx: 0.1352E-01 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 172.745 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.631(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 1 LOC: 90.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 58
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 22 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 19.71 32.40 0.608 Cl.D2 1 0.00 |
| TEN. RUPT. 19.71 32.40 0.608 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 22.50 0.000 Cl.E3 1 0.00 |
| FLEX. BUCK. V 0.000 7.571 0.000 Cl.E3 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.1056E-01 9.137 0.001 Cl.G1 1 0.00 |
| SHEAR Y 0.7257E-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 2.344 0.000 Cl.F10.1 1 3.75 |
| FLEX. YLD. V 0.2387E-01 1.064 0.022 Cl.F10.1 1 3.75 |
| L-T-B ABT U 0.2313E-17 1.679 0.000 Cl.F10.2 1 3.75 |
| F-L-B ABT U -.1156E-17 2.286 0.000 Cl.F10.3 1 1.25 |
| F-L-B ABT V -.4615E-03 1.038 0.000 Cl.F10.3 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.631 Eq.H2-1 1 3.75 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 59
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 23
|-----------------------------------------------------------------------------|
| Member No: 23 Profile: ST L30253 (AISC SECTIONS)|
| Status: PASS Ratio: 0.639 Loadcase: 1 |
| Location: 3.75 Ref: Eq.H2-1 |
| Pz: 19.97 T Vy: -.3351E-04 Vx: -.4876E-04 |
| Tz: 0.000 My: -.1950E-01 Mx: 0.1340E-01 |
|-----------------------------------------------------------------------------|
| TENSION SLENDERNESS |
| Actual Slenderness Ratio : 172.745 |
| Allowable Slenderness Ratio : 300.000 LOC : 0.00 |
|-----------------------------------------------------------------------------|
| STRENGTH CHECKS |
| Critical L/C : 1 Ratio : 0.639(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+: 2.642E-01 Sxx-: 2.628E-01 Zxx : 4.733E-01 |
| Syy+: 5.788E-01 Syy-: 6.814E-01 Zyy : 1.042E+00 |
| Cw : 7.100E-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.B4.1a.Case3 |
| Web : Slender 15.96 N/A 12.77 Table.B4.1a.Case3 |
| |
| FLEXURE CLASSIFICATION (L/C: 3 LOC: 90.00) |
| λ λp λr CASE |
| Flange: Compact 13.30 15.33 25.83 Table.B4.1b.Case12 |
| Web : NonCompact 15.96 15.33 25.83 Table.B4.1b.Case12 |
|-----------------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 60
STAAD.PRO CODE CHECKING - AISC 360-16 LRFD (V1.2)
*****************************************************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted).
- Member : 23 Contd.
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL TENSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| TEN. YLD. 19.97 32.40 0.616 Cl.D2 1 0.00 |
| TEN. RUPT. 19.97 32.40 0.616 Cl.D2 1 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL COMPRESSION |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| FLEX. BUCK. X 0.7236 20.27 0.036 Cl.E3 3 0.00 |
| FLEX. BUCK. Y 0.7236 15.51 0.047 Cl.E3 3 0.00 |
| FLEX. BUCK. U 0.7236 22.50 0.032 Cl.E3 3 0.00 |
| FLEX. BUCK. V 0.7236 7.571 0.096 Cl.E3 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR SHEAR |
|-----------------------------------------------------------------------------|
| DEMAND CAPACITY RATIO REFERENCE L/C LOC |
| |
| SHEAR X 0.1054E-01 9.137 0.001 Cl.G1 1 0.00 |
| SHEAR Y 0.7246E-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 2.344 0.000 Cl.F10.1 3 2.50 |
| FLEX. YLD. V 0.2366E-01 1.064 0.022 Cl.F10.1 1 3.75 |
| L-T-B ABT U -.1156E-17 1.516 0.000 Cl.F10.2 3 3.13 |
| F-L-B ABT U -.1156E-17 2.286 0.000 Cl.F10.3 3 3.13 |
| F-L-B ABT V -.1294E-02 1.038 0.001 Cl.F10.3 3 0.00 |
|-----------------------------------------------------------------------------|
| CHECKS FOR AXIAL BEND INTERACTION |
|-----------------------------------------------------------------------------|
| |
| RATIO CRITERIA L/C LOC |
| CLAUSE H2 0.639 Eq.H2-1 1 3.75 |
|-----------------------------------------------------------------------------|
93. STEEL TAKE OFF ALL
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 61
STEEL TAKE OFF
STEEL TAKE-OFF
--------------
PROFILE LENGTH(FEET) WEIGHT(KIP )
ST W14X90 55.00 4.950
ST W12X30 15.00 0.448
TC W21X50 30.00 4.182
ST W14X30 34.99 1.051
ST L30253 66.43 0.226
----------------
TOTAL = 10.857
************ END OF DATA FROM INTERNAL STORAGE ************
94. FINISH
*********** END OF THE STAAD.Pro RUN ***********
**** DATE= JUL 4,2024 TIME= 11:24:15 ****
EXAMPLE PROBLEM NO. 1 -- PAGE NO. 62
************************************************************
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* *
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************************************************************