1Beam configuration
2Section & material
0 to skip the pass/fail check

I = 4,166,666.7 mm⁴ · c = 50.00 mm

3Loads
1

Positive values act downward (point/distributed) or clockwise (moment).

Results
✓ Within allowable bending stress
Reaction A (pin)
2500.0N
Reaction B (roller)
2500.0N
Max moment
2500000.0N·mm
Max shear
2500.0N
Max deflection
-1.000mm
Max bending stress
30.0MPa
Beam schematic
defl.5,000 NL = 2000 mmloads shown positive-downward · not to scale
Shear force diagram
-3100.0-1550.00.01550.03100.0N0400800120016002000x (mm)
Bending moment diagram
-300000.0475000.01250000.02025000.02800000.0N·mm0400800120016002000x (mm)
Deflected shape
-1.120-0.810-0.500-0.1900.120mm0400800120016002000x (mm)
Reference & assumptions

New to Beam Theory? Read the guide: Beam Bending: Euler–Bernoulli Theory and Roark's Formulas — a plain-language explainer of the standard behind this calculator.

Assumes Euler-Bernoulli beam theory: a prismatic (uniform cross-section), linear-elastic, straight beam with small deflections, where plane sections remain plane. Statically determinate configurations (simply supported, cantilever, overhanging) are solved directly from static equilibrium; statically indeterminate configurations (fixed-fixed, propped-cantilever) are solved by the force (flexibility) method, using the unit-load / virtual-work theorem to enforce zero deflection/slope at the redundant support(s). Deflection is found by numerically double-integrating M(x)/EI. Results are cross-checked against the standard cases tabulated in Roark's Formulas for Stress and Strain (Table 3: shear, moment, slope, and deflection formulas for elastic straight beams). Shear/moment sign convention: upward reactions and sagging moments are positive; loads are entered positive-downward.

Validated: checked against Roark's closed-form cases for a 20×50 mm steel (E = 200 GPa) rectangular-section beam. Simply supported, 2000 mm span, 1000 N at midspan (Case: M = PL/4, δ = PL³/48EI) → this calculator returns M = 500,000 N·mm, δ = 4.00 mm, bending stress = 60.0 MPa, matching exactly. Cantilever, 1000 mm, 200 N at the tip (Case: M = PL at the fixed end, δ = PL³/3EI) → this calculator returns M = 200,000 N·mm, δ = 1.60 mm, bending stress = 24.0 MPa, also matching exactly.

Calculation steps
1. Support reactions
Static equilibrium: ΣFy = 0, ΣM = 0
Statically determinate
Reaction A (pin): 2500.0 N · Reaction B (roller): 2500.0 N
2. Maximum bending moment
M(x) — superposition of every load's contribution to the section moment
2500000.0 N·mm at x = 1000 mm
3. Maximum deflection
θ(x) = ∫M(x)/EI dx, y(x) = ∫θ(x) dx
EI = 200000 MPa × 4166666.7 mm⁴ = 8.333e+11 N·mm²
-1.000 mm at x = 1000 mm
4. Bending stress check
σ = M·c / I
σ = 2500000 N·mm × 50.00 mm / 4166666.7 mm⁴
30.0 MPa vs 250.0 MPa allowable — PASS