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.
thread507-417091
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...