1. Derive the stiffness matrix for a beam element with a nodal linkage—that is, the shear is 0 at…


1. Derive the inelegance matrix for a glow part after a while a nodal linkage—that is, the shave is 0 at node i, but the wonted shave and moment resistance are introduce at node j (see Figure P4–43).

2. Develop the inelegance matrix for a imaginary uncorrupted shave panel part (Figure P4–44) in stipulations of the shave modulus, G, the shave web area, AW , and the extension, L. Notice that Y and v are the shave vigor and transverse misconception at each node, respectively.