For the symmetric plane truss shown in Figure P3–35, determine (a) the deflection of node 1 and (b) the stress in element 1. AE/L for element 3 is twice AE=L for the other elements. Let AE/L = 106 lb/in. Then let A = 1 in2, L = 10 in., and E = 10 106 psi to obtain numerical results.
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