Can anybody help me to derive the expressions given here by unit load method? I was able to derive a,b and c. But the d and e are eccentric braced frames. I am stuck in that.
Yes but I am stuck in deriving the expressions given in the figure for eccentric braced frames. I do not know how to calculate the flexural component of deformation given by link element in eccentric braced frames while solving by unit load method.
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How do we calculate the shear deflection by unit load method for eccentric braced frames? I found the expression for first three frames. But I am not getting the expression for the remaining 2 frames. I am unable to find expression for deflection due to flexure in link and beam...
