Problem #2 The below cantilever beam is made from 6061 sheet…
Problem #2 The below cantilever beam is made from 6061 sheet annealed aluminum . The zero location of the beam is defined at the wall and the distance x is measured along the length of the beam from the zero location.E = 71.7GPa Assume that the length of the beam L = 0.800 m , a = 0.2 m, w = 800 N/m, F = 500 N, I = 2.50×10−8 m4, b = 0.7 m (NOTE: b is the distance from the zero location to where the force F is applied) You must evaluate the deflection at a distance 0.55m from the zero location. Represent all deflections as negative values.What is the contribution of the point load F to the overall beam deflection at 0.55m in units of m ? [F]mWhat is the contribution of the distributed load w to the overall beam deflection at 0.55m in units of m ? [w]mWhat is the overall beam deflection at 0.55m in units of m ? [total]m
Read Details