Simply supported beam carries uniformly distributed load shown in the following figure. The deflection, δ, along the beam is governed by the following equation:
δ = (5L^4x + 4Lx^3) / (384EI)
where:
x is the distance from the support A
L is the total length of the beam
w is the load per unit length
E is the Young modulus of the beam
I is the moment of inertia of the section of beam.
(Hint: W, L, E, and I are constant parameters)
Prove that:
The maximum deflection is at the mid-span of the beam, i.e. at x = L/2.
And the maximum deflection is (384EI / 5L^4).