Determine the equation for the deflection curve for the cantilever supported at A with a load given by: q=q0*sin([tex]\pi[/tex]x/L).
The Attempt at a Solution
I think this is pretty straightforward, but want to be sure. I did a similar problem with a simply supported beam with the same load equation, shown in the attached diagram. Am I safe to assume that the ONLY difference in this problem with a cantilever is the boundary conditions used to solve for C1, C2, etc?
The boundary conditions would be:
at x=0,y=0....and at x=0,moment=0.