Reference · Euler-Bernoulli
Beam deflection formulas
All cases assume linear-elastic, prismatic beams and small deflections. P = point load, w = load per length, L = span, E = modulus, I = inertia. Downward loads and deflection positive; sagging moment positive (cantilever hogging negative).
Simply supported
Off-center P at a: δ = Pb(L²−b²)3/2/9√3LEI · M = Pab/L @ a
Full UDL: δmax = 5wL⁴/384EI @ L/2 · M = wL²/8
End moment M₀: δ = M₀L²/16EI near mid · M(0⁺) = M₀
Two P at third points: δmax = 23PL³/648EI @ L/2
Cantilever (fixed wall)
P at a from wall: δP = Pa³/3EI · δtip = Pa²(3L−a)/6EI
Full UDL: δmax = wL⁴/8EI @ tip · Mwall = −wL²/2
Tip moment M₀: δtip = M₀L²/2EI
Fixed-fixed and propped
Fixed UDL: δmax = wL⁴/384EI · Mends = wL²/12, Mmid = wL²/24
Propped UDL: δmax ≈ wL⁴/185EI · Mwall = −wL²/8
Propped center P: δmax ≈ 7PL³/768EI
Stiffness ranking (same P, L, EI)
Fixed-fixed PL³/192EI (baseline, stiffest) → simply supported 4× softer → propped ≈ 6.8× → cantilever 64× softer. For UDL: fixed wL⁴/384EI → simply supported 5× → propped ≈ 2.1× → cantilever 48×. Boundary conditions dominate: doubling span multiplies point-load deflection 8× (L³) and UDL deflection 16× (L⁴).
Superposition
With P and UDL together, δtotal(x) = δP(x) + δw(x). Exact for linear-elastic small deflections — the calculator samples 121 stations and adds both fields, so peaks land correctly even off-center.