V. AISC LRFD - Non Compact Wide Flange 2
To determine the design bending strength of a non-compact American wide flange section bent about its strong axis. The deflection at mid-span due to two 10 kip concentrated loads acting at the third points along the beam is also to be calculated.
References
AISC Load Factor Resistance Design, 3rd Edition, Example 5.2, case (a), page 5-16.
Details
W21x48 shape
Calculations
Validation
Evaluate section for lateral-torsional buckling:
The plastic limiting unbraced length is given by:
Lb < Lp ; thus, the member is plastic.
Check flange slenderness:
Flanges are non-compact. The nominal moment capacity for the limit state of flange local buckling is:
The flange local buckling limit state capacity:
The ultimate moment is:
The capacity ratio is: 1,600 / 4,780 = 0.335
The deflection at mid-span for a beam loaded at third points:
Results
| Result Type | Reference | STAAD.Pro | Difference | Comments |
|---|---|---|---|---|
| Design flexural strength, ϕbMn (in·kips) | 4,780 |
4,780.24 |
negligible | |
| Capacity ratio | 0.335 | 0.335 | none | |
| Deflection (in) | 1.42 | 1.4114 | negligible |
Input
The file C:\Users\Public\Public Documents\STAAD.Pro 2026\Samples \Verification Models\09 Steel Design\US\AISC\AISC LRFD - Non Compact Wide Flange 2.STD is typically installed with the program.
The UNT 5 parameter specifies an unbraced length of 5'.
STAAD
STAAD SPACE BENDING CAPACITY PER AISC LRFD 3RD ED
START JOB INFORMATION
ENGINEER DATE 23-Sep-18
END JOB INFORMATION
*
* EXAMPLE PROBLEM 5.2, CASE (A), PAGE 5-16, AISC LRFD 3RD ED.
* CAPACITY (MNZ) SHOULD BE ABOUT 398 KIP-FT
*
UNIT FEET KIP
JOINT COORDINATES
1 0 0 0; 2 40 0 0;
*
MEMBER INCIDENCES
1 1 2;
*
MEMBER PROPERTY AMERICAN
1 TABLE ST W21X48
*
DEFINE MATERIAL START
ISOTROPIC MATERIAL1
E 4.176e+06
POISSON 0.3
END DEFINE MATERIAL
CONSTANTS
MATERIAL MATERIAL1 ALL
*
SUPPORTS
1 PINNED
2 FIXED BUT MZ
*
LOAD 1
MEMBER LOAD
1 CON GY -10 13.333
1 CON GY -10 26.667
*
PERFORM ANALYSIS
*
SECTION 0.5 ALL
PRINT SECTION DISPL
*
PARAMETER 1
CODE LRFD
MAIN 1 ALL
FYLD 7200 ALL
UNT 5 ALL
TRACK 1 ALL
CHECK CODE ALL
FINISH
Output
MEMBER SECTION DISPLACEMENTS
----------------------------
UNITS ARE - INCH
MEMB LOAD GLOBAL X,Y,Z DISPL FROM START TO END JOINTS AT 1/12TH PTS
1 1 0.0000 0.0000 0.0000 0.0000 -0.3644 0.0000
0.0000 -0.7057 0.0000 0.0000 -1.0010 0.0000
0.0000 -1.2273 0.0000 0.0000 -1.3654 0.0000
0.0000 -1.4114 0.0000 0.0000 -1.3654 0.0000
0.0000 -1.2273 0.0000 0.0000 -1.0010 0.0000
0.0000 -0.7057 0.0000 0.0000 -0.3644 0.0000
0.0000 0.0000 0.0000
MAX LOCAL DISP = 1.41141 AT 240.00 LOAD 1 L/DISP= 340
************ END OF SECT DISPL RESULTS ***********
40. *
41. PARAMETER 1
42. CODE LRFD
43. MAIN 1 ALL
44. FYLD 7200 ALL
45. UNT 5 ALL
46. TRACK 1 ALL
47. CHECK CODE ALL
STEEL DESIGN
BENDING CAPACITY PER AISC LRFD 3RD ED -- PAGE NO. 4
STAAD.Pro CODE CHECKING - (LRFD 3RD EDITION) v1.0
***********************
ALL UNITS ARE - KIP FEET (UNLESS OTHERWISE Noted)
MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/
FX MY MZ LOCATION
=======================================================================
1 ST W21X48 (AISC SECTIONS)
PASS LRFD-H1-1B-C 0.335 1
0.00 C 0.00 -133.33 13.33
+---------------------------------------------------------------------+
| DESIGN STRENGTHS FOR MEMBER 1 UNITS - KIP IN |
| PNC= 35.84 PNT= 634.50 MNZ= 4780.24 MNY= 636.75 VN= 194.67 |
+---------------------------------------------------------------------+