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Consider the Truss assembly given in below: a) Calculate elemental stiffness matrix. b) Compute global stiffness matrix. c) Apply boundary conditions and find reduced

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Consider the Truss assembly given in below: a) Calculate elemental stiffness matrix. b) Compute global stiffness matrix. c) Apply boundary conditions and find reduced stiffness matrix. d) Solve for nodal displacements at the node where Force F is applied E=200 GPa, A= 10 mm, Az= 500 mm, F=500N,L=200mm F L 60 30

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