| THEORY & FORMULAE |
Consider a simply-supported bar, having two concentrated forces acting vertically and located equidistant from each end of the beam. The following equations describe the distribution of shear force, bending moment and deformation:
    
where
     F = applied force at each load pointt
     L = length of beam or distance between supports
     a = location of load point from end of beam
     x = distance from left end of beam
     E = modulus of elasticity of beam material
     I = area moment of inertia of cross-sectional area about axis through centroid
     V = shear force
     M = bending moment
     D = deflection
     R1 = vertical reaction at left support
     R2 = vertical reaction at right support
     θ1 = angle of slope at left support
     θ2 = angle of slope at right support
The deflection at load point is given by D=[(Fa(3La -4a2)/6EI]. The maximum deflection is:
Dmax=[(Fa/24EI)*(3L2-4a2] occuring at x=L/2.
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