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Consider the bar in Fig.3.7 loaded as shown. Determine the nodal displacements, element stresses, and support reactions. Solv

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A= 4UDMY A >250 W E 2UDXJ0 Stepl Divide GVen gemety the 2 element D*creti2tion into ot geemetry C.S L.c.s 2. 2 2 3 2 2 lo baf2.6 2.6 2.6 2.C 4 Step3 letaltrutura Ltiffnes is assembly-f k, k^^ k3 matrix 2.2 32 2.2 3233 -2.3 -3.3 2-3+2E 2.6 -2.6 2 422ЗФо XI03 С.602 Зоох03 3.303 ,- Зxlо 6.6U2 3.203 = 2xjo *лg - 3.302+Sq02 сд luution 2 6.211F, U2 3.Sxlo mm

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