# EX. UK-1 Plane Frame with Steel Design

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

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

where:
• L = 4.5 m, H1 = 6.0 m, H2 = 4.5 m, and H 3 = 2.7 m
• WLx = 9.0 KN/m, WLy = 15 KN/m, RL = 13.5 KN/m, LL = 17.5 KN/m, P1 = 135 KN, P2 = 35 KN
• Members 1, 3, & 4 are a UC356X368X129, Members 5, 6, & 7 are a UB533X210X82, Member 2 is a UC254X254X73, Members 8 through 13 are a UB457X152X52. All other members comprising the truss are a UA100X100X8

Actual input is shown in bold lettering followed by explanation.

`   STAAD PLANE EXAMPLE PROBLEM NO. 1`

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

`   UNIT METER KN`

Defines the input units for the data that follows.

```   JOINT COORDINATES
1 0 0 ; 2 9 0 ; 3 0 6 ; 4 3 6
5 6 6 ; 6 9 6 ; 7 0 10.5
8 9 10.5 ; 9 2.25 10.5 ; 10 6.75 10.5
11 4.5 10.5 ; 12 1.5 11.4 ; 13 7.5 11.4
14 3 12.3 ; 15 6 12.3 ; 16 4.5 13.2```

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

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

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

```   MEMBER PROPERTY BRITISH
1 3 4 TA ST UC356X368X129 ; 2 TA ST UC254X254X73
5 6 7 TA ST UB533X210X82 ; 8 TO 13 TA ST UB457X152X52
14 TO 23 TA ST UA100X100X8```

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

```   MEMB TRUSS
14 TO 23```

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

```   MEMB RELEASE
5 START MZ```

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

```   UNIT KNS MMS
DEFINE MATERIAL START
ISOTROPIC STEEL
E 210
POISSON 0.3
DENSITY 7.68191e-008
ALPHA 6e-006
DAMP 0.03
TYPE STEEL
STRENGTH FY 0.24821 FU 0.399894 RY 1.5 RT 1.2
END DEFINE MATERIAL```

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

```   CONSTANTS
BETA 90.0 MEMB 3 4
MATERIAL STEEL ALL
UNIT METER```

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

```   SUPPORT
1 FIXED ; 2 PINNED```

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

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

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

`   LOADING 1 DEAD AND LIVE LOAD`

Load case 1 is initiated followed by a title.

`   SELFWEIGHT Y -1.0`

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

```   JOINT LOAD
4 5 FY -65. ; 11 FY -155.```

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 -13.5 ; 6 UNI GY -17.5```

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

`   CALCULATE RAYLEIGH FREQUENCY`

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

```   LOADING 2 WIND FROM LEFT
1 2 UNI GX 9.0 ; 8 TO 10 UNI Y -15.0```

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

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

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

This command instructs the program to proceed with the analysis.

`   LOAD LIST 1 3`

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

```   PRINT MEMBER FORCES
PRINT SUPPORT REACTION```

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

```   PARAMETER
CODE EN 1993-1-1:2005
NA 1
NSF 0.85 ALL
BEAM 1 ALL
KY 1.2 MEMB 3 4
RATIO 0.9 ALL```

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

`   SELECT ALL`

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

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

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

`   PERFORM ANALYSIS`

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

```   PARAMETER
BEAM 1.0 ALL
RATIO 1.0 ALL
TRACK 1.0 ALL ```

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

`   CHECK CODE ALL`

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

`   STEEL TAKE OFF`

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

`   FINISH`

This command terminates the STAAD run.

## Input File

``````STAAD PLANE EXAMPLE PROBLEM NO. 1
UNIT METER KN
JOINT COORDINATES
1 0. 0. ; 2 9. 0. ; 3 0. 6. ; 4 3. 6.
5 6. 6. ; 6 9. 6. ; 7 0 10.5
8 9. 10.5 ; 9 2.25 10.5 ; 10 6.75 10.5
11 4.5 10.5 ; 12 1.5 11.4 ; 13 7.5 11.4
14 3. 12.3 ; 15 6. 12.3 ; 16 4.5 13.2
MEMBER INCIDENCE
1 1 3 ; 2 3 7 ; 3 2 6 ; 4 6 8 ; 5 3 4
6 4 5 ; 7 5 6 ; 8 7 12 ; 9 12 14
10 14 16 ; 11 15 16 ; 12 13 15 ; 13 8 13
14 9 12 ; 15 9 14 ; 16 11 14 ; 17 11 15
18 10 15 ; 19 10 13 ; 20 7 9
21 9 11 ; 22 10 11 ; 23 8 10
MEMBER PROPERTY BRITISH
1 3 4 TA ST UC356X368X129 ; 2 TA ST UC254X254X73
5 6 7 TA ST UB533X210X82 ; 8 TO 13 TA ST UB457X152X52
14 TO 23 TA RA UA100X100X8
*MEMB TRUSS
*14 TO 23
MEMB RELEASE
5 START MZ
14 to 23 start MPY 0.99 MPZ 0.99
14 to 23 end MPY 0.99 MPZ 0.99
UNIT KNS MMS
DEFINE MATERIAL START
ISOTROPIC STEEL
E 210
POISSON 0.3
DENSITY 7.68191e-008
ALPHA 6e-006
DAMP 0.03
TYPE STEEL
STRENGTH FY 0.24821 FU 0.399894 RY 1.5 RT 1.2
END DEFINE MATERIAL
CONSTANTS
MATERIAL STEEL ALL
BETA 90.0 MEMB 3 4
UNIT METER
SUPPORT
1 FIXED ; 2 PINNED
PRINT MEMBER INFORMATION LIST 1 5 14
PRINT MEMBER PROPERTY LIST 1 2 5 8 14
SELFWEIGHT Y -1.0
4 5 FY -65. ; 11 FY -155.
8 TO 13 UNI Y -13.5 ; 6 UNI GY -17.5
CALCULATE RAYLEIGH FREQUENCY
1 2 UNI GX 9.0 ; 8 TO 10 UNI Y -15.0
* 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
PRINT MEMBER FORCES
PRINT SUPPORT REACTION
PARAMETER
CODE EN 1993-1-1:2005
NA 1
NSF 0.85 ALL
BEAM 3 ALL
KY 1.2 MEMB 3 4
RATIO 0.9 ALL
SELECT ALL
GROUP MEMB 1 3 4
GROUP MEMB 5 6 7
GROUP MEMB 8 TO 13
GROUP MEMB 14 TO 23
PERFORM ANALYSIS
PARAMETER
BEAM 3 ALL
RATIO 1.0 ALL
TRACK 1.0 ALL
CHECK CODE ALL
STEEL TAKE OFF
FINISH
``````

```                                                                  PAGE NO.    1
****************************************************
*                                                  *
*           Version  22.08.00.***                  *
*           Proprietary Program of                 *
*           Bentley Systems, Inc.                  *
*           Date=    OCT 19, 2021                  *
*           Time=    17:53:23                      *
*                                                  *
*  Licensed to: Bentley Systems Inc                *
****************************************************
1. STAAD PLANE EXAMPLE PROBLEM NO. 1
INPUT FILE: UK-1 Plane Frame with Steel Design.STD
2. UNIT METER KN
3. JOINT COORDINATES
4. 1 0. 0. ; 2 9. 0. ; 3 0. 6. ; 4 3. 6.
5. 5 6. 6. ; 6 9. 6. ; 7 0 10.5
6. 8 9. 10.5 ; 9 2.25 10.5 ; 10 6.75 10.5
7. 11 4.5 10.5 ; 12 1.5 11.4 ; 13 7.5 11.4
8. 14 3. 12.3 ; 15 6. 12.3 ; 16 4.5 13.2
9. MEMBER INCIDENCE
10. 1 1 3 ; 2 3 7 ; 3 2 6 ; 4 6 8 ; 5 3 4
11. 6 4 5 ; 7 5 6 ; 8 7 12 ; 9 12 14
12. 10 14 16 ; 11 15 16 ; 12 13 15 ; 13 8 13
13. 14 9 12 ; 15 9 14 ; 16 11 14 ; 17 11 15
14. 18 10 15 ; 19 10 13 ; 20 7 9
15. 21 9 11 ; 22 10 11 ; 23 8 10
16. MEMBER PROPERTY BRITISH
17. 1 3 4 TA ST UC356X368X129 ; 2 TA ST UC254X254X73
18. 5 6 7 TA ST UB533X210X82 ; 8 TO 13 TA ST UB457X152X52
19. 14 TO 23 TA RA UA100X100X8
20. *MEMB TRUSS
21. *14 TO 23
22. MEMB RELEASE
23. 5 START MZ
24. 14 TO 23 START MPY 0.99 MPZ 0.99
25. 14 TO 23 END MPY 0.99 MPZ 0.99
26. UNIT KNS MMS
27. DEFINE MATERIAL START
28. ISOTROPIC STEEL
29. E 210
30. POISSON 0.3
31. DENSITY 7.68191E-008
32. ALPHA 6E-006
33. DAMP 0.03
34. TYPE STEEL
35. STRENGTH FY 0.24821 FU 0.399894 RY 1.5 RT 1.2
36. END DEFINE MATERIAL
37. CONSTANTS
38. MATERIAL STEEL ALL
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    2
39. BETA 90.0 MEMB 3 4
40. UNIT METER
41. SUPPORT
42. 1 FIXED ; 2 PINNED
43. 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        (METE)     (DEG)     RELEASES
1        1       3           6.000     0.00
5        3       4           3.000     0.00    000001000000
14        9      12           1.172     0.00    000011000011
************ END OF DATA FROM INTERNAL STORAGE ************
44. PRINT MEMBER PROPERTY LIST 1 2 5 8 14
MEMBER   PROPERTY LIST     1
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    4
MEMBER PROPERTIES. UNIT - CM
-----------------
MEMB   PROFILE              AX/          IZ/          IY/        IX/
AY           AZ           SZ         SY
1  ST  UC356X368X129
164.00     40200.00     14600.00      152.61
36.98       116.11      2260.97      792.19
2  ST  UC254X254X73      93.10     11400.00      3910.00       57.62
21.85        65.07       897.28      307.15
5  ST  UB533X210X82     105.00     47500.00      2010.00       51.52
50.72        49.61      1798.22      192.53
8  ST  UB457X152X52      66.60     21400.00       645.00       21.37
34.18        29.90       951.53       84.65
14  RA  UA100X100X8       15.50       236.82        59.54        3.31
5.33         5.33        33.49       15.20
************ END OF DATA FROM INTERNAL STORAGE ************
46. SELFWEIGHT Y -1.0
48. 4 5 FY -65. ; 11 FY -155.
50. 8 TO 13 UNI Y -13.5 ; 6 UNI GY -17.5
51. CALCULATE RAYLEIGH FREQUENCY
54. 1 2 UNI GX 9.0 ; 8 TO 10 UNI Y -15.0
55. * 1/3 RD INCREASE IS ACCOMPLISHED BY 75% LOAD
56. LOAD COMB 3 75 PERCENT DL LL WL
57. 1 0.75 2 0.75
58. PERFORM ANALYSIS
P R O B L E M   S T A T I S T I C S
-----------------------------------
NUMBER OF JOINTS         16  NUMBER OF MEMBERS      23
NUMBER OF PLATES          0  NUMBER OF SOLIDS        0
NUMBER OF SURFACES        0  NUMBER OF SUPPORTS      2
Using 64-bit analysis engine.
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    5
SOLVER USED IS THE IN-CORE ADVANCED MATH SOLVER
TOTAL      PRIMARY LOAD CASES =     2, TOTAL DEGREES OF FREEDOM =      43
TOTAL LOAD COMBINATION  CASES =     1  SO FAR.
**********************************************************
*                                                        *
* MAX DEFLECTION =  2.54900 CM   GLO X,  AT JOINT     7  *
*                                                        *
**********************************************************
60. PRINT MEMBER FORCES
MEMBER   FORCES
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    6
MEMBER END FORCES    STRUCTURE TYPE = PLANE
-----------------
ALL UNITS ARE -- KNS  METE     (LOCAL )
MEMBER  LOAD  JT     AXIAL   SHEAR-Y  SHEAR-Z   TORSION     MOM-Y      MOM-Z
1    1     1    239.70     -7.78     0.00      0.00      0.00     -72.75
3   -232.14      7.78     0.00      0.00      0.00      26.08
3     1    179.63     85.56     0.00      0.00      0.00     334.46
3   -173.96    -45.06     0.00      0.00      0.00      57.40
2    1     3    150.33    -22.49     0.00      0.00      0.00     -26.08
7   -147.12     22.49     0.00      0.00      0.00     -75.14
3     3    128.83     -0.18     0.00      0.00      0.00     -57.40
7   -126.42     30.56     0.00      0.00      0.00     -11.77
3    1     2    258.31      0.00    -7.78      0.00      0.00       0.00
6   -250.75      0.00     7.78      0.00     46.67       0.00
3     2    244.50      0.00   -15.69      0.00      0.00       0.00
6   -238.83      0.00    15.69      0.00     94.14       0.00
4    1     6    142.80      0.00   -22.49      0.00     71.03       0.00
8   -137.13      0.00    22.49      0.00     30.19       0.00
3     6    141.64      0.00   -60.93      0.00    140.17       0.00
8   -137.39      0.00    60.93      0.00    134.03       0.00
5    1     3    -14.72     81.80     0.00      0.00      0.00       0.00
4     14.72    -79.38     0.00      0.00      0.00     241.78
3     3    -45.24     45.12     0.00      0.00      0.00       0.00
4     45.24    -43.31     0.00      0.00      0.00     132.65
6    1     4    -14.72     14.38     0.00      0.00      0.00    -241.78
5     14.72     40.54     0.00      0.00      0.00     202.55
3     4    -45.24     -5.44     0.00      0.00      0.00    -132.65
5     45.24     46.63     0.00      0.00      0.00      54.55
7    1     5    -14.72   -105.54     0.00      0.00      0.00    -202.55
6     14.72    107.96     0.00      0.00      0.00    -117.70
3     5    -45.24    -95.38     0.00      0.00      0.00     -54.55
6     45.24     97.19     0.00      0.00      0.00    -234.31
8    1     7    167.81     70.72     0.00      0.00      0.00      75.13
12   -167.35    -46.34     0.00      0.00      0.00      27.25
3     7    172.82     43.62     0.00      0.00      0.00      11.77
12   -172.47     -5.65     0.00      0.00      0.00      31.33
9    1    12    168.29     40.04     0.00      0.00      0.00     -27.24
14   -167.83    -15.66     0.00      0.00      0.00      75.96
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    7
MEMBER END FORCES    STRUCTURE TYPE = PLANE
-----------------
ALL UNITS ARE -- KNS  METE     (LOCAL )
MEMBER  LOAD  JT     AXIAL   SHEAR-Y  SHEAR-Z   TORSION     MOM-Y      MOM-Z
3    12    167.89     34.90     0.00      0.00      0.00     -31.32
14   -167.55      3.06     0.00      0.00      0.00      59.17
10    1    14    188.07    -88.15     0.00      0.00      0.00     -75.98
16   -187.61    112.53     0.00      0.00      0.00     -99.54
3    14    154.06    -61.65     0.00      0.00      0.00     -59.19
16   -153.71     99.62     0.00      0.00      0.00     -81.86
11    1    15    188.04    -88.20     0.00      0.00      0.00     -76.06
16   -187.58    112.58     0.00      0.00      0.00     -99.54
3    15    160.58    -70.47     0.00      0.00      0.00     -57.40
16   -160.23     88.75     0.00      0.00      0.00     -81.86
12    1    13    182.56     36.30     0.00      0.00      0.00     -33.87
15   -182.10    -11.92     0.00      0.00      0.00      76.05
3    13    123.15     38.74     0.00      0.00      0.00      -5.61
15   -122.80    -20.45     0.00      0.00      0.00      57.39
13    1     8    184.91     48.81     0.00      0.00      0.00      30.19
13   -184.45    -24.43     0.00      0.00      0.00      33.87
3     8    118.55     88.96     0.00      0.00      0.00     134.01
13   -118.21    -70.68     0.00      0.00      0.00       5.62
14    1     9     -6.25      0.05     0.00      0.00      0.00       0.00
12      6.36      0.04     0.00      0.00      0.00       0.01
3     9     29.69      0.04     0.00      0.00      0.00      -0.00
12    -29.61      0.03     0.00      0.00      0.00       0.01
15    1     9      4.86      0.05     0.00      0.00      0.00      -0.00
14     -4.64      0.04     0.00      0.00      0.00       0.01
3     9    -24.97      0.04     0.00      0.00      0.00      -0.00
14     25.13      0.03     0.00      0.00      0.00       0.01
16    1    11   -107.59      0.08     0.00      0.00      0.00      -0.01
14    107.80      0.10     0.00      0.00      0.00      -0.01
3    11    -44.00      0.06     0.00      0.00      0.00      -0.01
14     44.16      0.07     0.00      0.00      0.00      -0.01
17    1    11    -94.66      0.08     0.00      0.00      0.00      -0.01
15     94.87      0.10     0.00      0.00      0.00      -0.01
3    11   -107.68      0.06     0.00      0.00      0.00      -0.01
15    107.84      0.07     0.00      0.00      0.00      -0.01
18    1    10    -10.44      0.05     0.00      0.00      0.00      -0.00
15     10.66      0.04     0.00      0.00      0.00       0.01
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    8
MEMBER END FORCES    STRUCTURE TYPE = PLANE
-----------------
ALL UNITS ARE -- KNS  METE     (LOCAL )
MEMBER  LOAD  JT     AXIAL   SHEAR-Y  SHEAR-Z   TORSION     MOM-Y      MOM-Z
3    10     26.57      0.04     0.00      0.00      0.00      -0.00
15    -26.41      0.03     0.00      0.00      0.00       0.01
19    1    10     12.13      0.05     0.00      0.00      0.00       0.00
13    -12.02      0.04     0.00      0.00      0.00       0.01
3    10    -32.23      0.04     0.00      0.00      0.00       0.00
13     32.31      0.03     0.00      0.00      0.00       0.01
20    1     7    -85.02      0.14     0.00      0.00      0.00       0.01
9     85.02      0.13     0.00      0.00      0.00       0.00
3     7    -95.19      0.10     0.00      0.00      0.00      -0.00
9     95.19      0.10     0.00      0.00      0.00       0.00
21    1     9    -90.88      0.14     0.00      0.00      0.00       0.00
11     90.88      0.13     0.00      0.00      0.00       0.01
3     9    -66.58      0.10     0.00      0.00      0.00      -0.00
11     66.58      0.10     0.00      0.00      0.00       0.01
22    1    10    -99.16      0.14     0.00      0.00      0.00      -0.00
11     99.16      0.13     0.00      0.00      0.00       0.01
3    10    -25.81      0.10     0.00      0.00      0.00       0.00
11     25.81      0.10     0.00      0.00      0.00       0.01
23    1     8   -110.95      0.14     0.00      0.00      0.00       0.00
10    110.95      0.13     0.00      0.00      0.00       0.00
3     8      5.05      0.11     0.00      0.00      0.00       0.02
10     -5.05      0.09     0.00      0.00      0.00      -0.00
************** END OF LATEST ANALYSIS RESULT **************
61. PRINT SUPPORT REACTION
SUPPORT  REACTION
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.    9
SUPPORT REACTIONS -UNIT KNS  METE    STRUCTURE TYPE = PLANE
-----------------
JOINT  LOAD   FORCE-X   FORCE-Y   FORCE-Z     MOM-X     MOM-Y     MOM Z
1    1      7.78    239.70      0.00      0.00      0.00    -72.75
3    -85.56    179.63      0.00      0.00      0.00    334.46
2    1     -7.78    258.31      0.00      0.00      0.00      0.00
3    -15.69    244.50      0.00      0.00      0.00      0.00
************** END OF LATEST ANALYSIS RESULT **************
62. PARAMETER
63. CODE EN 1993-1-1:2005
64. NA 1
65. NSF 0.85 ALL
66. BEAM 3 ALL
67. KY 1.2 MEMB 3 4
68. RATIO 0.9 ALL
69. SELECT ALL
STEEL DESIGN
STAAD.PRO MEMBER SELECTION - BS EN 1993-1-1:2005
********************************************
NATIONAL ANNEX - NA to BS EN 1993-1-1:2005
PROGRAM CODE REVISION V1.14 BS_EC3_2005/1
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   10
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
1 ST  UC305X305X118(BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.868         3
179.63 C          0.00         334.46        0.00
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
2 ST  UC203X203X46 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.882         1
147.12 C          0.00         -75.14        4.50
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
3 ST  UC254X254X89 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.736         3
238.83 C         94.14           0.00        6.00
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
4 ST  UC305X305X97 (BRITISH SECTIONS)
PASS     EC-6.2.9.1         0.822         3
141.64 C        140.17           0.00        0.00
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   11
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
5 ST  UB457X191X67 (BRITISH SECTIONS)
PASS     EC-6.3.2 LTB       0.863         1
14.72 T          0.00         241.78        3.00
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
6 ST  UB457X191X67 (BRITISH SECTIONS)
PASS     EC-6.3.2 LTB       0.883         1
14.72 T          0.00        -247.42        0.75
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
7 ST  UB457X191X67 (BRITISH SECTIONS)
PASS     EC-6.3.2 LTB       0.836         3
45.24 T          0.00        -234.31        3.00
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
8 ST  UB356X127X33 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.844         1
167.81 C          0.00          75.13        0.00
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   12
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
9 ST  UB254X146X37 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.855         1
167.83 C          0.00          75.96        1.75
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
10 ST  UB406X140X39 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.803         1
187.61 C          0.00         -99.54        1.75
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
11 ST  UB406X140X39 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.803         1
187.58 C          0.00         -99.54        1.75
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
12 ST  UB254X146X37 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.870         1
182.10 C          0.00          76.05        1.75
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   13
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
13 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.851         3
118.55 C          0.00         134.01        0.00
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
14 RA  UA50x50x4    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.780         3
29.68 C          0.00          -0.00        0.10
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
15 RA  UA35x35x4    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.865         1
4.75 C          0.00          -0.03        0.98
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
16 RA  UA65x50x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.871         1
107.69 T          0.00          -0.05        1.17
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   14
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
17 RA  UA65x50x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.862         3
107.76 T          0.00          -0.04        1.17
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
18 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.783         3
26.57 C          0.00          -0.00        0.00
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
19 RA  UA35x35x4    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.832         1
12.07 C          0.00          -0.02        0.68
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
20 RA  UA60x40x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.897         3
95.19 T          0.00          -0.06        1.12
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   15
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
21 RA  UA60x40x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.875         1
90.88 T          0.00          -0.08        1.12
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
22 RA  UA65x50x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.826         1
99.16 T          0.00          -0.08        1.13
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
23 RA  UA60x40x6    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.888         1
110.95 T          0.00          -0.08        1.12
************** END OF TABULATED RESULT OF DESIGN **************
70. GROUP MEMB 1 3 4
GROUPING BASED ON MEMBER      1  (ST  UC305X305X118   ) LIST=      1....
71. GROUP MEMB 5 6 7
GROUPING BASED ON MEMBER      7  (ST  UB457X191X67    ) LIST=      5....
72. GROUP MEMB 8 TO 13
GROUPING BASED ON MEMBER     13  (ST  UB356X171X45    ) LIST=      8....
73. GROUP MEMB 14 TO 23
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   16
GROUPING BASED ON MEMBER     18  (RA  UA60x60x5       ) LIST=     14....
74. PERFORM ANALYSIS
** ALL CASES BEING MADE ACTIVE BEFORE RE-ANALYSIS. **
**********************************************************
*                                                        *
* MAX DEFLECTION =  4.57423 CM   GLO X,  AT JOINT     7  *
*                                                        *
**********************************************************
75. PARAMETER
76. BEAM 3 ALL
77. RATIO 1.0 ALL
78. TRACK 1.0 ALL
79. CHECK CODE ALL
STEEL DESIGN
STAAD.PRO CODE CHECKING - BS EN 1993-1-1:2005
********************************************
NATIONAL ANNEX - NA to BS EN 1993-1-1:2005
PROGRAM CODE REVISION V1.14 BS_EC3_2005/1
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   17
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
1 ST  UC305X305X118(BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.910         3
178.79 C          0.00         351.35        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     1 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  460.6 MCY=  210.3 PC=  2285.0 PT=  3525.0 MB=  410.5 PV=  582.9|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  3525.00    FX/PZ =   0.05       MRZ=  460.6      MRY=  210.3   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
2 ST  UC203X203X46 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.802         1
144.94 C          0.00         -68.59        4.50
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     2 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  116.8 MCY=   54.3 PC=   800.0 PT=  1379.5 MB=   98.9 PV=  229.9|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1379.45    FX/PZ =   0.11       MRZ=  116.8      MRY=   54.3   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
3 ST  UC305X305X118(BRITISH SECTIONS)
PASS     EC-6.2.9.1         0.438         3
235.25 C         92.19           0.00        6.00
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   18
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     3 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  460.6 MCY=  210.3 PC=  1930.8 PT=  3525.0 MB=  410.5 PV=  582.9|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  3525.00    FX/PZ =   0.07       MRZ=  460.6      MRY=  210.3   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
4 ST  UC305X305X118(BRITISH SECTIONS)
PASS     EC-6.2.9.1         0.659         3
138.96 C        138.54           0.00        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     4 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  460.6 MCY=  210.3 PC=  2466.9 PT=  3525.0 MB=  438.0 PV=  582.9|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  3525.00    FX/PZ =   0.04       MRZ=  460.6      MRY=  210.3   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
5 ST  UB457X191X67 (BRITISH SECTIONS)
PASS     EC-6.3.2 LTB       0.861         1
14.61 T          0.00         241.23        3.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     5 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  345.5 MCY=   55.7 PC=  1485.4 PT=  2009.3 MB=  280.1 PV=  555.4|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  2009.25    FX/PZ =   0.01       MRZ=  345.5      MRY=   55.7   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   19
6 ST  UB457X191X67 (BRITISH SECTIONS)
PASS     EC-6.3.2 LTB       0.882         1
14.61 T          0.00        -246.94        0.75
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     6 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  345.5 MCY=   55.7 PC=  1485.4 PT=  2009.3 MB=  280.1 PV=  555.4|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  2009.25    FX/PZ =   0.01       MRZ=  345.5      MRY=   55.7   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
7 ST  UB457X191X67 (BRITISH SECTIONS)
PASS     EC-6.3.2 LTB       0.824         3
44.31 T          0.00        -230.73        3.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     7 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  345.5 MCY=   55.7 PC=  1485.4 PT=  2009.3 MB=  280.1 PV=  555.4|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  2009.25    FX/PZ =   0.02       MRZ=  345.5      MRY=   55.7   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
8 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.512         1
165.72 C          0.00          68.59        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     8 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  182.1 MCY=   34.5 PC=  1193.5 PT=  1346.6 MB=  175.5 PV=  363.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1346.55    FX/PZ =   0.12       MRZ=  182.1      MRY=   34.5   |
|---------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   20
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
9 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.573         1
166.04 C          0.00          77.15        1.75
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB     9 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  182.1 MCY=   34.5 PC=  1193.5 PT=  1346.6 MB=  175.5 PV=  363.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1346.55    FX/PZ =   0.12       MRZ=  182.1      MRY=   34.5   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
10 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.682         1
186.60 C          0.00         -97.18        1.75
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    10 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  182.1 MCY=   34.5 PC=  1193.5 PT=  1346.6 MB=  175.5 PV=  363.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1346.55    FX/PZ =   0.14       MRZ=  182.1      MRY=   34.5   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
11 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.682         1
186.46 C          0.00         -97.18        1.75
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    11 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  182.1 MCY=   34.5 PC=  1193.5 PT=  1346.6 MB=  175.5 PV=  363.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1346.55    FX/PZ =   0.14       MRZ=  182.1      MRY=   34.5   |
|---------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   21
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
12 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.584         1
175.61 C          0.00          77.56        1.75
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    12 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  182.1 MCY=   34.5 PC=  1193.5 PT=  1346.6 MB=  175.5 PV=  363.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1346.55    FX/PZ =   0.13       MRZ=  182.1      MRY=   34.5   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
13 ST  UB356X171X45 (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.831         3
121.12 C          0.00         130.01        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    13 UNIT - kN,m  SECTION CLASS  1  |
|MCZ=  182.1 MCY=   34.5 PC=  1193.5 PT=  1346.6 MB=  175.5 PV=  363.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.127    K =  1.000  |
| PZ=  1346.55    FX/PZ =   0.09       MRZ=  182.1      MRY=   34.5   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
14 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.285         3
19.99 C          0.00           0.00        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    14 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    75.6 PT=   136.8 MB=    1.9 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.15       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   22
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
15 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.174         1
5.91 C          0.00          -0.00        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    15 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    35.3 PT=   136.8 MB=    1.6 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.04       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
16 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.797         1
105.96 T          0.00          -0.02        1.17
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    16 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    25.5 PT=   136.8 MB=    1.5 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.77       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
17 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.781         3
104.19 T          0.00          -0.01        1.17
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   23
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    17 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    25.5 PT=   136.8 MB=    1.5 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.76       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
18 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.3.3-662       0.670         3
22.72 C          0.00          -0.00        0.00
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    18 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    35.3 PT=   136.8 MB=    1.6 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.17       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
19 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.206         3
27.43 T          0.00          -0.00        0.59
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    19 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    75.6 PT=   136.8 MB=    1.9 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.20       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   24
20 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.639         1
83.85 T          0.00          -0.03        1.12
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    20 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    27.4 PT=   136.8 MB=    1.5 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.61       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
21 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.691         1
90.76 T          0.00          -0.03        1.12
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    21 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    27.4 PT=   136.8 MB=    1.5 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.66       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
22 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.738         1
97.10 T          0.00          -0.03        1.13
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    22 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    27.4 PT=   136.8 MB=    1.5 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.71       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   25
ALL UNITS ARE - KNS  METE (UNLESS OTHERWISE Noted)
FX            MY             MZ       LOCATION
=======================================================================
23 RA  UA60x60x5    (BRITISH SECTIONS)
PASS     EC-6.2.9.2/3       0.774         1
101.92 T          0.00          -0.03        1.12
|---------------------------------------------------------------------|
| CALCULATED CAPACITIES FOR MEMB    23 UNIT - kN,m  SECTION CLASS  4  |
|MCZ=    1.5 MCY=    0.8 PC=    27.4 PT=   136.8 MB=    1.5 PV=   27.1|
| BUCKLING  CO-EFFICIENTS C1  AND  K  :    C1 =  1.132    K =  1.000  |
| PZ=   136.77    FX/PZ =   0.75       MRZ=    1.5      MRY=    0.8   |
|---------------------------------------------------------------------|
************** END OF TABULATED RESULT OF DESIGN **************
80. STEEL TAKE OFF
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   26
STEEL TAKE OFF
STEEL TAKE-OFF
--------------
PROFILE                 LENGTH(METE)      WEIGHT(KNS )
ST  UC305X305X118               16.50            19.013
ST  UC203X203X46                 4.50             2.029
ST  UB457X191X67                 9.00             5.911
ST  UB356X171X45                10.50             4.620
RA  UA60x60x5                   19.93             0.891
----------------
TOTAL =         32.464
************ END OF DATA FROM INTERNAL STORAGE ************
81. FINISH
*********** END OF THE STAAD.Pro RUN ***********
**** DATE= OCT 19,2021   TIME= 17:53:24 ****
EXAMPLE PROBLEM NO. 1                                    -- PAGE NO.   27
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```