Bending Stress Calculator

Find bending stress from moment and section, and check it against yield.

Please note: These are idealised textbook models using representative material data. They are for study, sizing and sanity-checking only — never for final design. Real engineering requires code-compliant analysis, verified material certificates and a qualified engineer’s sign-off.

What the Bending Stress Calculator does

Bending stress is the moment divided by the section modulus — a single number describing how efficiently a shape resists bending. Because the section modulus already folds in both the shape’s stiffness and how far its outer fibres sit from the neutral axis, comparing sections is just comparing that one figure.

Formula

  • σ = M ÷ S
  • S = I ÷ c
  • M capacity = σ_allowable × S
  • Safety factor = Yield strength ÷ σ

Inputs explained

InputUnitRequiredNotes
Solve forone of 2 optionsYes
Bending momentkN·mIn some modesAccepts more than 0. Shown in 5 of the 10 modes.
Allowable stressMPaIn some modesAccepts more than 0. Shown in 5 of the 10 modes.
Materialone of 13 optionsYes
Cross-sectionone of 5 optionsYes
WidthnumberIn some modesShown in 6 of the 10 modes.
Width unitone of 9 optionsIn some modesShown in 6 of the 10 modes.
Height / depthnumberIn some modesShown in 6 of the 10 modes.
Height / depth unitone of 9 optionsIn some modesShown in 6 of the 10 modes.
Outer diameternumberIn some modesShown in 4 of the 10 modes.
Outer diameter unitone of 9 optionsIn some modesShown in 4 of the 10 modes.
Inner diameternumberIn some modesShown Solve for is Stress from a known moment and Cross-section is Round tube (hollow circle), or Solve for is Moment the section can carry and Cross-section is Round tube (hollow circle).
Inner diameter unitone of 9 optionsIn some modesShown Solve for is Stress from a known moment and Cross-section is Round tube (hollow circle), or Solve for is Moment the section can carry and Cross-section is Round tube (hollow circle).
Wall thicknessnumberIn some modesShown Solve for is Stress from a known moment and Cross-section is Rectangular hollow section, or Solve for is Moment the section can carry and Cross-section is Rectangular hollow section.
Wall thickness unitone of 9 optionsIn some modesShown Solve for is Stress from a known moment and Cross-section is Rectangular hollow section, or Solve for is Moment the section can carry and Cross-section is Rectangular hollow section.
Flange thicknessnumberIn some modesShown Solve for is Stress from a known moment and Cross-section is I-beam / wide flange, or Solve for is Moment the section can carry and Cross-section is I-beam / wide flange.
Flange thickness unitone of 9 optionsIn some modesShown Solve for is Stress from a known moment and Cross-section is I-beam / wide flange, or Solve for is Moment the section can carry and Cross-section is I-beam / wide flange.
Web thicknessnumberIn some modesShown Solve for is Stress from a known moment and Cross-section is I-beam / wide flange, or Solve for is Moment the section can carry and Cross-section is I-beam / wide flange.
Web thickness unitone of 9 optionsIn some modesShown Solve for is Stress from a known moment and Cross-section is I-beam / wide flange, or Solve for is Moment the section can carry and Cross-section is I-beam / wide flange.
Required safety factornumberOptionalAccepts 0.1 or more.

How to use it

  1. Choose Solve for and Material.
  2. Fill in the remaining inputs the form shows for your choice.
  3. Optionally add Required safety factor.
  4. Select Calculate.

Worked example

A 5.625 kN·m moment on a 100 × 200 mm steel rectangle.

Moment
5.625 kN·m
Section
100 × 200 mm
Material
Structural steel

S = 666,667 mm³, so σ = 5,625 ÷ 0.000667 = 8.44 MPa. Against 250 MPa yield that is a safety factor of 29.6.

Frequently asked questions

What is section modulus?

Second moment of area divided by the distance to the extreme fibre. It captures a shape’s bending resistance in one number, so stress is simply moment divided by it.

Why are I-beams shaped that way?

Bending stress is proportional to distance from the neutral axis, so material at the centre does almost nothing. Moving it into flanges far from the axis buys stiffness for very little weight.

Method and sources

Method. Bending stress as moment over section modulus, σ = M ÷ S, with the section modulus derived from the geometry entered.

Assumptions

  • Plane sections remain plane, the material is linear-elastic, and bending is about a principal axis.

Limitations

  • Valid below the elastic limit only; beyond yield the linear distribution this assumes no longer holds.
  • Stress concentrations at holes, notches and section changes are not modelled and can multiply local stress several times.
  • Combined loading — bending with torsion or axial force — needs the stresses combined, which this does not do.

Sources

  • The design code governing the component, and classical beam bending theory — Varies by jurisdiction and material. The permissible stress and safety factors. The stress relationship itself is standard mechanics of materials.

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