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Engineering · Mechanics of Materials

Beam Bending Stress Calculator

Maximum bending stress in a beam from the flexure formula σ = M·c ÷ I.

Input method
kN·m
Maximum moment at the section, in kN·m.
mm
Neutral axis to the outermost fibre.
mm⁴
Second moment of area; scientific notation OK.
Worked examples — tap to load
Maximum bending stress (σ)
60MPa

Tension on one face, equal compression on the other. Section modulus S = 83330 mm³, so σ = M ÷ S. 1 MPa = 1 N/mm².

Maximum bending stress is the flexure formula σ = M·c ÷ I = M ÷ S, where M is the bending moment, c the distance to the extreme fibre, I the area moment of inertia, and S = I ÷ c the section modulus. A 5 kN·m moment on a 50 × 100 mm rectangle (I = 4.167×10⁶ mm⁴, c = 50 mm) gives σ = 60 MPa.

What bending stress is

When a beam bends, the material on one face is stretched while the opposite face is squeezed. Somewhere between them lies the neutral axis — a layer that is neither in tension nor compression and carries no bending stress at all. The stress grows linearly with distance from that axis, so the largest values sit at the extreme fibres, the surfaces farthest from the neutral axis. The flexure formula turns the internal bending moment M into that peak stress using the section’s geometry.

σ = M·c ÷ I = M ÷ S

σ = bending stress, M = bending moment, c = distance from the neutral axis to the extreme fibre, I = area moment of inertia, S = I ÷ c = section modulus. Use N·mm and mm so σ comes out in MPa (N/mm²).

Worked example

A rectangular beam 50 mm wide and 100 mm deep carries a maximum bending moment of 5 kN·m. For a rectangle, I = b·h³ ÷ 12 = 50 × 100³ ÷ 12 = 4.167×10⁶ mm⁴, and c is half the depth, 50 mm.

  1. 1
    Find the maximum bending moment. Take M at the section of interest — usually where the moment peaks. Here M = 5 kN·m = 5×10⁶ N·mm. Working in N·mm and mm makes σ come out in MPa.
  2. 2
    Locate the neutral axis and the extreme fibre. For a symmetric section the neutral axis passes through the centroid, so c is half the depth: c = 100 ÷ 2 = 50 mm.
  3. 3
    Get the area moment of inertia I. For a rectangle, I = b·h³ ÷ 12 = 50 × 100³ ÷ 12 = 4.167×10⁶ mm⁴. Use the Area Moment of Inertia tool for other shapes.
  4. 4
    Compute the section modulus (optional). S = I ÷ c = 4.167×10⁶ ÷ 50 = 83,333 mm³. Bending tables often list S directly, letting you skip straight to σ = M ÷ S.
  5. 5
    Apply the flexure formula. σ = M·c ÷ I = 5×10⁶ × 50 ÷ 4.167×10⁶ = 60 MPa. Equivalently σ = M ÷ S = 5×10⁶ ÷ 83,333 = 60 MPa.

Unit combinations that give σ in MPa

Bending stress in MPa (N/mm²) needs consistent units. Mixing N·m with mm inflates σ by 1000, so convert the moment first.

M (moment)c and I (or S)Result σ
N·mmc in mm, I in mm⁴MPa (N/mm²) directly
kN·mmultiply by 1×10⁶ → N·mmMPa after converting M
N·mmS in mm³ (S = I ÷ c)MPa via σ = M ÷ S
N·mc in m, I in m⁴Pa — divide by 1×10⁶ for MPa

Reading and using the result

The flexure formula assumes pure bending of a straight, prismatic beam made of a linear-elastic material, with plane sections staying plane. Under those conditions the top and bottom fibres see equal and opposite stresses on a symmetric section — one in tension, one in compression. Compare the peak σ against the material’s allowable stress (yield strength divided by a factor of safety) to judge whether the section is adequate.

Because σ depends on c ÷ I, pushing material away from the neutral axis is the most effective way to cut stress: it raises I faster than c, so the section modulus S climbs and σ falls. That is exactly why I-beams concentrate area in the flanges. This calculator handles the bending stress once M is known; finding M itself, and the resulting deflection, are separate steps.

What is the neutral axis?
It is the layer inside a bending beam that is neither stretched nor compressed, so the bending stress there is zero. For a symmetric cross-section it passes through the centroid. Bending stress grows linearly with distance from this axis, reaching its maximum at the extreme fibres.
What units give bending stress in MPa?
Enter the moment in N·mm, and c and I in mm and mm⁴ (or S in mm³); then σ comes out in N/mm², which equals MPa exactly. This tool takes M in kN·m and multiplies by 1×10⁶ to reach N·mm for you.
What is the section modulus S?
S = I ÷ c combines the area moment of inertia and the extreme-fibre distance into one number, so the flexure formula simplifies to σ = M ÷ S. Beam tables list S directly, which is why it is handy for quick checks.
How is bending stress different from axial stress?
Axial stress σ = F ÷ A is uniform across the section from a direct pull or push. Bending stress varies linearly across the depth — zero at the neutral axis, peak at the extreme fibres — because it comes from a moment, not a straight force.
Why do the extreme fibres see the maximum stress?
Bending stress is proportional to distance from the neutral axis, σ = M·y ÷ I. The extreme fibres are the farthest points, at y = c, so they carry the largest tension on one face and the largest compression on the other.
Where do I get the area moment of inertia I?
I depends only on the cross-section shape. For a rectangle I = b·h³ ÷ 12; for a circle I = π·d⁴ ÷ 64. Use the Area Moment of Inertia tool for standard sections, then bring that value here.
Does this formula work past the yield point?
No. σ = M·c ÷ I assumes linear-elastic behaviour. Once the extreme fibres yield, stress no longer varies linearly across the depth, and plastic-bending analysis with the plastic section modulus is needed instead.