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Space truss

Description

A statically indeterminate cantilever space truss as shown below, loaded with a joint load and a uniform temperature load.

Geometry

Modulus of Elasticity: 30,000 ksi
Thermal coefficient: 11.7×10-6 (in/in)/°C
Elements: beam elements, Area: 1.0 in²
Supports: Pinned

Loads

Joint load FX2 (node 6) = -1.0
Axial temperature change = +27.8°C (all beams)

Reference

S. P. Timoshenko & D. H. Young, Theory of Structures, Second Edition. (article 7.6, problems 1,2), McGraw – Hill book company.

Comparison of Results

Beam Load Result type Result Deviation
Theoretical STRAP
4 Joint Axial 0.056 0.056
4 Temperature Axial 1.295 1.294 0.07%

 

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