A simply supported beam of length 6 m is subjected to a uniformlydistributed load w = 10 kN/m, as shown in Figure 2(a). The cross-section dimensions of the beam are shown in Figure 2(b). Assume thattwisting does not occur in the beam. Determine the bending stressdistribution in the cross-section at location A in the beam. The sectionhas a constant thickness t = 1 mm. Thin-walled assumptions apply(ignore terms with ³).200010035(a)40X135100(b)w = 10 kN/m4000All dimensions are inmillimetre (mm)40

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A simply supported beam of length 6 m is subjected to a uniform distributed load w = 10 kN/m, as shown in Figure 2(a). The cros section dimensions of the beam are shown in Figure 2(b). Assume th twisting does not occur in the beam. Determine the bending stre distribution in the cross-section at location A in the beam. The secti has a constant thickness t = 1 mm. Thin-walled assumptions app (ignore terms with t³). w = 10 kN/m

A simply supported beam of length 6 m is subjected to a uniform distributed load w = 10 kN/m, as shown in Figure 2(a). The cros section dimensions of the beam are shown in Figure 2(b). Assume th twisting does not occur in the beam. Determine the bending stre distribution in the cross-section at location A in the beam. The secti has a constant thickness t = 1 mm. Thin-walled assumptions app (ignore terms with t³). w = 10 kN/m

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Concept explainers

Matrix Algebra for Structural analysis

Structural analysis is a process in which the effects of different loads and internal forces, acting on structures and their elements are determined. This method of analysis is effective in detecting the failure loads of the structural elements and the design can be altered before commencing the construction process, which ensures proper strength and safety of the structures.

Question

A simply supported beam of length 6 m is subjected to a uniformly
distributed load w = 10 kN/m, as shown in Figure 2(a). The cross-
section dimensions of the beam are shown in Figure 2(b). Assume that
twisting does not occur in the beam. Determine the bending stress
distribution in the cross-section at location A in the beam. The section
has a constant thickness t = 1 mm. Thin-walled assumptions apply
(ignore terms with ³).
2000
100
35
(a)
40
X1
35
100
(b)
w = 10 kN/m
4000
All dimensions are in
millimetre (mm)
40

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