UNDERSTAND IT. WORK IT OUT.

Learn: Beam shear stress

Shear force does not normally produce a uniform stress over a beam cross-section. This formula finds the local shear stress at a chosen level by using the area on one side of that level.

Beginner-friendlyFree · No accountTwo worked examples + separate practice
01

What the formula is saying

Q is the first moment of that partial area about the neutral axis. VQ describes the change in bending force that must be transferred; dividing by I and the local width converts it to shear stress.

τ = V Q / (I b)

Read the symbols in plain language

V
Shear force

Shear force. Multiply the section shear force by the first moment for the chosen level.

N

Newtons measure force; 1000 N = 1 kN.

Q
First moment of area

Area on one side of the shear-evaluation level multiplied by its centroid’s distance from the neutral axis; this is Q, not I.

m³

Cubic metres measure volume, or a first moment of area where explicitly identified.

I
Second moment of area

The area-weighted square of distance from the stated axis. It measures the spread of the cross-section, not its area or mass.

m⁴

The fourth power of metres is used for a second moment of area; 1 m⁴ = 10¹² mm⁴.

b
Width at evaluation point

Width at evaluation point. The full-section second moment and local width control the stress distribution.

m

Metres measure length; 1 m = 1000 mm.

τ
Result to find

Beam shear stress. Divide to obtain force per unit area at the selected location.

Pa

Sort out the units first

Use N, m³, m⁴ and m for V, Q, I and b. The units reduce to N/m² = Pa. Q is not a force or the full section’s second moment.

Assumptions before calculating

The beam is straight, slender and prismatic; E and I are constant. Deflections are small and Euler–Bernoulli bending applies: shear deformation, joint flexibility and geometric nonlinearity are neglected.

02

Let’s solve one together

Read the given values, follow each operation, then check what the result means.

Read the supplied values as one complete study case. Find τ and explain the result in the stated output unit.

V · Shear force
100000 N
Q · First moment of area
0.002 m³
I · Second moment of area
0.005 m⁴
b · Width at evaluation point
0.3 m
  1. Form the shear-transfer numerator

    Multiply the section shear force by the first moment for the chosen level.

    (100000) × (0.002) = 200 N·m³
  2. Build the geometric divisor

    The full-section second moment and local width control the stress distribution.

    (0.005) × (0.3) = 0.0015 m⁵
  3. Calculate local shear stress

    Divide to obtain force per unit area at the selected location.

    (200) ÷ (0.0015) ≈ 133333.3333 Pa
Answer133333.3333 Pa

Does this worked answer make sense?

At a free top or bottom surface Q is zero, so this ideal shear stress is zero. Increasing local width with all other inputs fixed reduces the stress.

A second worked example — different values

A second case uses different data. Predict which way the answer will change, then calculate it without reusing the first answer.

V · Shear force
50000 N
Q · First moment of area
0.001 m³
I · Second moment of area
0.002 m⁴
b · Width at evaluation point
0.2 m
  1. Form the shear-transfer numerator

    Multiply the section shear force by the first moment for the chosen level.

    (50000) × (0.001) = 50 N·m³
  2. Build the geometric divisor

    The full-section second moment and local width control the stress distribution.

    (0.002) × (0.2) = 0.0004 m⁵
  3. Calculate local shear stress

    Divide to obtain force per unit area at the selected location.

    (50) ÷ (0.0004) = 125000 Pa
Answer125000 Pa
03

Now try your own values

Change a value or its unit. The same method will show your calculation, step by step.

Shear force. Multiply the section shear force by the first moment for the chosen level.

Area on one side of the shear-evaluation level multiplied by its centroid’s distance from the neutral axis; this is Q, not I.

The area-weighted square of distance from the stated axis. It measures the spread of the cross-section, not its area or mass.

Width at evaluation point. The full-section second moment and local width control the stress distribution.

English, Arabic and Persian digits are supported. The steps convert inputs to the formula’s base units.

Results update only when you calculate. The lesson example above stays unchanged.

04

Your turn — check your understanding

Solve this separate case yourself. Use only the values below; the two worked examples use different data. Give the requested result in the selected unit.

V · Shear force
80000 N
Q · First moment of area
0.0015 m³
I · Second moment of area
0.004 m⁴
b · Width at evaluation point
0.25 m

Find: Learn: Beam shear stress

For repeating decimals, use at least four significant figures. Accepted rounding tolerance: 0.05% of the expected value; zero uses an absolute tolerance of 10⁻¹².

A hint, not the answer

Q is the first moment of that partial area about the neutral axis. VQ describes the change in bending force that must be transferred; dividing by I and the local width converts it to shear stress.

Use N, m³, m⁴ and m for V, Q, I and b. The units reduce to N/m² = Pa. Q is not a force or the full section’s second moment.

Show the full practice solution

Compare the steps with your work; revealing a solution does not mark the lesson complete.

  1. Form the shear-transfer numerator

    Multiply the section shear force by the first moment for the chosen level.

    (80000) × (0.0015) = 120 N·m³
  2. Build the geometric divisor

    The full-section second moment and local width control the stress distribution.

    (0.004) × (0.25) = 0.001 m⁵
  3. Calculate local shear stress

    Divide to obtain force per unit area at the selected location.

    (120) ÷ (0.001) = 120000 Pa
Answer120000 Pa

Avoid the common trap

Use width at the evaluation point, not automatically the flange width. Build Q from the correct partial area and centroid distance; do not replace it with I.

When this method applies — and when it does not

This elementary formula applies where beam theory describes the stress distribution. Local concentrations near supports, holes, load introduction and abrupt thickness changes need separate assessment.

For study and understanding, not approval of a real structure, site operation or design. Apply the correct standard, National Annex and professional review to actual engineering work.

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Sources & further reading

References open in a new tab and explain the underlying principles. The teaching text and examples here are SimpleFlick’s own; the source organisations have not endorsed this calculator.

Reading focus: Beam shear stress. Use the relevant elastic-response, equilibrium, constitutive-relations or shear-and-torsion module; the lesson states its particular sign convention.

Lesson updated: · Both examples and the separate practice case are checked against an independent high-precision numerical implementation. This verifies arithmetic for the stated model, not engineering certification.

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