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A simply supported beam of length L is subjected to linearly varying load, w: Figure 5. The bending moment, M, of the beam is expressed as M =" (x³ – 1²x) Given that dx2 M where El > 0 is the constant flexural rigidity of the be deflection, y, for the initial conditions at x = 0, y = 0, = 0 and x = L, y = dx

A simply supported beam of length L is subjected to linearly varying load, w: Figure 5. The bending moment, M, of the beam is expressed as M =" (x³ – 1²x) Given that dx2 M where El > 0 is the constant flexural rigidity of the be deflection, y, for the initial conditions at x = 0, y = 0, = 0 and x = L, y = dx

Structural Analysis
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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A simply supported beam of length L is subjected to linearly varying load, wx, as shown in Figure 5. The bending moment, M, of the beam is expressed as M =" (x³ – 1²x) M Given that dx2 where El > 0 is the constant flexural rigidity of the beam, derive the deflection, y, for the initial conditions at x = 0, y = 0, = 0 and x = L, y = 0. W Figure 5
Transcribed Image Text:A simply supported beam of length L is subjected to linearly varying load, wx, as shown in Figure 5. The bending moment, M, of the beam is expressed as M =" (x³ – 1²x) M Given that dx2 where El > 0 is the constant flexural rigidity of the beam, derive the deflection, y, for the initial conditions at x = 0, y = 0, = 0 and x = L, y = 0. W Figure 5
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