`theta_1 = theta_2 = (omega * l^3)/(24 * E*I)`

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Beam Simply Supported at Ends uniformly distributed load ω(N/M)   can be expressed as:

    `theta_1 = theta_2 = (`omega`*l^3)/(24*E*I)`

    where

  
     E = modulus of elasticity (Pa (N/`m^2`), N/`mm^2`, psi)
   
     I = moment of Inertia (`m^4`,`"mm"^4`, `"in"^4`)

    l = Length of beam(m)

This equation computes cantilever beam that is uniformly distributed load `omega`.