Q4. Determine the joint displacements, support reactions, and member axial forces for the 3D truss shownbelow using the flexibility method.ZYALx12(2)34PLzLyEA = 1 × 105 kN for all membersLx= 10 mLy10 mLz = 10 mP = 10 kN=Q4.{Ua}= =-8-8-1:7-={Ps}-8-8-={p} ==R₁xR₁yRızR3xR3yR3zRAXRAYRAZ||kN-100 kNT0m

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Q4. Determine the joint displacements, support reactions, and member axial forces for the 3D truss shown below using the flexibility method. Lx YA 1 3 P Ly EA = 1 x 105 kN for all members Lx = 10 m Ly = 10 m L₂ = 10 m P = 10 KN Q4. U₂) }}-{}={8} - 0 m {Ua} = U₂=U3 = {p} = P₂ = (R₁x) R₁y R₁z R3x {Ps} = R3y R32 RAX RAY RAZ 0 KN II 0 KN

Q4. Determine the joint displacements, support reactions, and member axial forces for the 3D truss shown below using the flexibility method. Lx YA 1 3 P Ly EA = 1 x 105 kN for all members Lx = 10 m Ly = 10 m L₂ = 10 m P = 10 KN Q4. U₂) }}-{}={8} - 0 m {Ua} = U₂=U3 = {p} = P₂ = (R₁x) R₁y R₁z R3x {Ps} = R3y R32 RAX RAY RAZ 0 KN II 0 KN

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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