Beam Stress and Deflection Moment Equations and Calculator Beam Supported Partial Distributed Uniform loading Applied

Beam Deflection and Stress Formula and Calculators

Area Moment of Inertia Equations & Calculators

Stress Deflection Moment Equations and Calculator Beam Supported Distributed Uniform Loading Applied

Structural Beam Deflection, Shear and Stress Equations and calculator for a Beam supported One End Cantilevered with Reversed Tapered Load.

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Preview Calculator: Beam Stress and Deflection Moment Calculator Beam Supported Partial Distributed Uniform loading Applied


Reaction and Shear Equation

Reaction and Shear Equation


Bending Moments Equation

Bending Moments Equation


Deflection and End Slope Equation

Deflection and End Slope Equation


Where:

E = Modulus of Elasticity psi

(N/mm2)

I = Moment of Inertia in4 (mm4)
W = Load, Total lbf (N)
w = Unit Load lbs/in (N/mm)
y = Deflection inches (mm)
a, b, c, d, x, L = Some distance as indicated inches (mm)
n = Distance neutral axis inches (mm)
Vmax = Shear Load lbf (N)
Mmax = Moment lbs-in (N-mm)
θmax = Slope Angle degree (radian)
σmax = Stress max. psi (N/mm2)
  • Deflections apply only to constant cross sections along entire length.

References:

  • Boeing Design Manual, Rev G. 1994 BDM

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