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The simply supported beam AB in Figure 1 is subjected to a load variation given by w(x) = -kr. ܨܝ܂ Figure 1 (a) Determine th

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Detailed solution has been given below. However, this problem has a lot principles applied into it. Though, I have explained almost everything, but still if any confusion or even a tiniest doubt arises, feel free to put that in the comments section, i'll be happy to help you out with it.

Page sal Lets first calculate the total load on the beam D В. Lets take a element of dr_thickness, at a distance I from beParze NC Som adding al..the moments, EMO KL Rip La=0 5 ܕܩ 5 Ro. - K44 5 Also, due to vertical W = RATRB equilibrium ftranslatNow, we koow EI dy da M() K24x K5 Eldy dr2 5 20 Integrałng_above equahon on both sides, we get: EI dy da Kl4r? 10 Kx5 HG 120Putting values of Good (2.11 ev lewe get EIY = KL73 30 Kr? 840 27 KLCC 890 ANS Lei Ya 28 KL 3. K527- 27 KLOK 640 EI bo_he_er

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