V. Thermal Loading on a Beam
To find the support reactions due to a temperature loads applied on a fixed-fixed beam.
References
Hand calculation using the following reference:
Matrix Analysis of Framed Structures, 3rd edition, W.Weaver Jr. & J.M.Gere, Van Nostrand Reinhold, Table B2, Appendix B, p.500
Details
The beam in the following geometric, load, and section properties: L = 7.5 m, α =
11.7(10)-6/°F,
IZ = 5,000 cm4
, E =200 KN/mm2
, A = 50 cm2
.
- Case 1: T = 40° F (uniform across section)
- Case 2: T1 = 0° F (below beam), T2 = 50° F (above beam)
Calculations
Theoretical Solution
Horizontal reactions due to case 1 loads:
RA = - RB = EAαΔT =
[200(10)6]×[50(10)-4]×[11.7(10)-6]· (40) = 468
kN
Moment reactions due to case 2 loads:
Results
| Result Type | Theory | STAAD.Pro | Difference |
|---|---|---|---|
| Horizontal Reaction at Node A (kN) | 468 | 468 | none |
| Moment at Node A (kN·m) | 19.5 | 19.5 | none |
Note: In the STAAD.Pro model, two load cases
are used. In case 1, the uniform expansion is applied. In case 2, the temperature change
between top and bottom flanges is applied.
Input
The file C:\Users\Public\Public Documents\STAAD.Pro 2026\Samples \Verification Models\01 Beams\Thermal Loading on a Beam.STD is typically installed with the program.
STAAD
STAAD PLANE TEMPERATURE LOAD ON A FIXED-FIXED BEAM
START JOB INFORMATION
ENGINEER DATE 18-Sep-18
END JOB INFORMATION
*
* REFERENCE : MATRIX ANALYSIS OF FRAMED STRUCTURES
* GERE & WEAVER, 3RD EDITION, VAN NOSTRAND REINHOLD
*
* TABLE B-2, APPENDIX B, PAGE 500
*
UNIT METER KN
JOINT COORDINATES
1 0 0 0; 2 3 0 0; 3 7.5 0 0;
MEMBER INCIDENCES
1 1 2; 2 2 3;
UNIT CM KN
MEMBER PROPERTY AMERICAN
1 2 PRIS AX 50 IZ 5000 YD 30
UNIT METER KN
DEFINE MATERIAL START
ISOTROPIC MATERIAL1
E 2e+08
POISSON 0.3
ALPHA 1.17e-05
END DEFINE MATERIAL
CONSTANTS
MATERIAL MATERIAL1 ALL
SUPPORTS
1 FIXED
3 FIXED
LOAD 1
TEMPERATURE LOAD
1 2 TEMP 40
LOAD 2
TEMPERATURE LOAD
1 2 TEMP 0 50
PERFORM ANALYSIS
PRINT SUPPORT REACTION
FINISHOutput
SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE
-----------------
JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z
1 1 468.00 0.00 0.00 0.00 0.00 0.00
2 0.00 0.00 0.00 0.00 0.00 -19.50
3 1 -468.00 0.00 0.00 0.00 0.00 0.00
2 0.00 0.00 0.00 0.00 0.00 19.50