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Beam Load & Deflection Calculator

Simply supported beam — max moment, max shear, max deflection, and bending stress under a centered point load or uniformly distributed load.

Max deflection (mid-span)
— L/x
Max moment
in-lb
Max shear
lb
Bending stress
psi
Section modulus
in³
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How a simply supported beam responds to load

A simply supported beam is the basic case: pinned at one end, roller at the other, free to deflect downward under load. The maximum bending moment, shear, and deflection all occur at predictable points depending on how the load is applied.

Center point load (P at mid-span)

M_max = P × L / 4 (at mid-span) V_max = P / 2 (at supports) δ_max = P × L³ / (48 × E × I) (at mid-span)

Uniformly distributed load (w, lb per linear inch)

M_max = w × L² / 8 (at mid-span) V_max = w × L / 2 (at supports) δ_max = 5 × w × L⁴ / (384 × E × I)

Bending stress

σ = M / S S = I / c (c = distance from neutral axis to outer fiber)

For a rectangle with width b and depth h: I = bh³/12, S = bh²/6. Doubling depth multiplies I by 8 and S by 4 — depth always wins over width.

Deflection limits (IBC Table 1604.3)

The calculator above reports the deflection ratio so you can compare directly. δ < L/360 is generally serviceable for floor framing.

Modulus of elasticity (typical values)

Frequently asked questions

Deflection formula?
Center point: PL³/(48EI). UDL: 5wL⁴/(384EI).
Max floor deflection?
L/360 live load, L/240 total per IBC Table 1604.3.
What is moment of inertia?
Stiffness in bending. Rectangle: I = bh³/12. Doubling depth multiplies I by 8.
Bending stress?
σ = M/S. Compare to material allowable: 24 ksi A36, ~1,500 psi DFL Select Structural.

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