bending calculator

Beam Bending Calculator (Rectangular Section)

Use this tool to estimate maximum bending stress and deflection for common beam loading cases. Units are set to N and mm for consistent engineering calculations.

Typical steel value: 200000 MPa. Typical aluminum value: 69000 MPa.
Enter applied point load in Newtons.

What this bending calculator does

This bending calculator provides fast estimates for beam behavior under load. It computes the second moment of area for a rectangular cross-section, then uses classic beam formulas from strength of materials to report:

  • Maximum bending moment
  • Maximum bending stress
  • Maximum deflection
  • Deflection ratio (L/δ), often used for serviceability checks

It is ideal for concept design, quick engineering checks, classroom exercises, and early-stage sizing decisions before detailed finite element modeling or code compliance verification.

Inputs explained

1) Load case

Choose the structural support and loading condition that matches your setup:

  • Simply supported + center load: supports at both ends with one point load at midspan.
  • Cantilever + end load: fixed at one end with load applied at the free end.
  • Simply supported + UDL: load spread evenly across the full span.

2) Geometry (L, b, h)

The tool assumes a rectangular cross-section. Width and height strongly influence stiffness: because the inertia includes , increasing section height has a dramatic effect on reducing deflection and stress.

3) Elastic modulus (E)

Elastic modulus defines how stiff the material is. Higher E means less deflection for the same load and geometry. Be sure to use consistent units; here, E is in MPa (which is numerically N/mm²).

Equations used

The calculator uses the following formulas for a rectangular beam:

  • Second moment of area: I = b·h³/12
  • Section modulus: S = I/(h/2)
  • Bending stress: σ = M/S

Maximum moment and deflection depend on load case:

  • Simply supported, center point load: M = P·L/4, δ = P·L³/(48·E·I)
  • Cantilever, end point load: M = P·L, δ = P·L³/(3·E·I)
  • Simply supported, full-span UDL: M = w·L²/8, δ = 5·w·L⁴/(384·E·I)

How to use results responsibly

Treat this tool as a preliminary calculator. Real beams can fail or deform due to effects not included here: shear deformation, local buckling, lateral-torsional buckling, notches, temperature effects, dynamic loading, and inelastic behavior.

If your design is safety-critical, always verify with the proper engineering standard, required safety factors, and detailed structural analysis.

Practical design tips

  • Increasing beam depth is usually the most efficient way to cut deflection.
  • Material change (higher E) helps stiffness, but geometry often gives bigger gains.
  • Check both strength (stress limit) and serviceability (deflection limit).
  • For long spans, deflection usually governs before stress.
  • Keep units consistent—unit mistakes are one of the most common causes of bad calculations.

Example workflow

Suppose you have a simply supported steel beam, 1000 mm long, with a 50 mm by 100 mm rectangular section and a center load of 1000 N. Enter those values directly into the calculator, then compare the output stress against your allowable material stress and compare deflection ratio against your project criterion (for example, L/240 or L/360).

If the deflection is too high, try increasing h first. If stress is too high, increase section modulus (again, often by increasing height) or reduce the load/span.

🔗 Related Calculators