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Shear Stress Calculator

Table of contents

Transverse shear stress formulaTorsional shear stress equation - Shear stress due to torsionImportant considerations when using this calculator and the shear stress equationsFAQs

This shear stress calculator calculates the shear stress due to transverse loads and the shear stress due to torsion (torque) applied on a circular shaft.

The shear stress from transverse forces is critical in the design of thin-walled members. For non-tin-walled members subjected to transverse loads, the most important is usually the axial stress caused by the bending moment. Our stress calculator can also be helpful if you're dealing with axial stress. If that's not the case, use this calculator!

The shear stress equation to use will depend on whether we apply a transverse load to a beam or a torsion couple to a circular shaft. In the following sections, you can look at the formulas for shear stress under these two conditions. We'll show how to calculate the maximum shear stress for many beams and how to calculate the stress at any point.

Transverse shear stress formula

By definition, shear stress is force acting tangent to an area. In a beam of cross-sectional area AA subjected to a shear force (VV), the average shear stress (τavg\tau_\text{avg}) is:

τavg=VA\tau_\text{avg} = \frac{V}{A}

This is just an average, as the shear stress across a beam subjected to transverse shear varies widely, and we usually need to know its maximum value instead of just the average.

You can find the exact shear stress at any vertical distance from the neutral axis with the following equation:

τ=VQIt\tau = \frac{VQ}{It}


  • τ\tau – Shear stress at a specific distance from the neutral axis;
  • VV – Internal shear force at the section of interest in the beam;
  • QQ – First moment (about the neutral axis) of the cross-sectional area that lies above the point where we'll calculate the stress;
  • tt – Section width at the point where we'll calculate the shear stress; and
  • II – Moment of inertia of the entire cross-sectional area, about the neutral axis (you can find it with our moment of inertia calculator).

QQ is a tricky quantity. Mathematically, it is the area above the point of interest multiplied by the distance between the centroid of that area to the neutral axis. For example, for the cross-section of cam geometry below, if you wanted to calculate the shear stress at a distance yy' from the neutral axis, the corresponding QQ would be Q=yˉAˉQ = \bar y' \bar A.

Image of a beam with cam cross-section geometry.

Using the shear formula (τ=VQ/It\tau = VQ/It) requires being careful about calculating the different quantities (especially QQ) and carefully inspecting the point of maximum shear stress (τmax\tau_\text{max}). For that reason, in this calculator, we included the possibility of obtaining τmax\tau_\text{max} for the most common shapes (rectangular, circular, and I-beams) by only inputting their dimensions and the shear force. You can look at those formulas in the table below (scroll to the right to look at them):


Maximum shear stress


Image of a rectangular section and its dimensions

τmax=3V2A\tau_\text{max} = \frac{3V}{2A}

A=dbA = db

Stress at distance y:

τ=3V2A(1y2(d/2)2)\tau = \frac{3V}{2A}(1-\frac{y^2}{(d/2)^2})

Hollow circle

Image of a hollow circular section and its dimensions

τmax=4V3AR2+RRi+Ri2R2+Ri2\tau_\text{max} = \frac{4V}{3A}\frac{R^2+RR_i+{R_i}^2}{R^2+{R_i}^2}

A=π(R2Ri2)A = \pi(R^2 - R_i^2)


Image of a wide-flange beam section and its dimensions

τmax=V8 Ixt(b(d+2t)2bd2+td2)\tau_\text{max} = \frac{V}{8\ I_xt} \left(b(d+2t)^2 - bd^2+td^2\right)

τmin=Vb8 Ixt((d+2t)2d2)\tau_\text{min} = \frac{Vb}{8\ I_xt} \left((d+2t)^2 - d^2\right)

I=b(d+2t)3(bt)d312I = \frac{b(d+2t)^3-(b-t)d^3}{12}

💡 In an I-beam (wide-flange beam), the τmin\tau_\text{min} value (the stress value at the joint between the flange and web) is a critical quantity, as sometimes the joint in that zone is created through welding or glue, and we need to calculate how much stress those elements will withstand.

Torsional shear stress equation - Shear stress due to torsion

To calculate the shear stress from a torque applied to a circular shaft, we use the torsional shear stress formula:

τ=TρJ\tau = \frac{T \rho}{J}


  • τ\tau – Shear stress at the point of interest;
  • ρ\rho – Radial distance from the shaft center to the point where we want to calculate the stress (the point of interest);
  • TT – Torque applied to the shaft; and
  • JJ – Polar moment of inertia of the cross-section.
    • For a solid shaft of radius RR, J=πR4/2J = \pi R^4/2.
    • For a hollow shaft of inner radius RiR_\text i and outer radius RR, J=π(R4Ri4)/2J = \pi(R^4 - {R_\text i}^4)/2.
    You can calculate JJ with our polar moment of inertia calculator.

The maximum shear stress for torsional loads occurs at the outer surface of the circular shaft, where ρ=R\rho = R. In other words, the maximum shear stress (τmax\tau_\text{max}) is given by:

τmax=TRJ\tau_\text{max} = \frac{TR}{J}

Important considerations when using this calculator and the shear stress equations

Please keep this in mind:

  • When using these formulas (and most of the formulas in mechanics of materials), you must consider that they apply to homogenous materials with a linear elastic behavior.
  • When we apply a transverse load to a beam, transverse and longitudinal shear stresses arise. Due to the complementary property of shear, these longitudinal and transversal stresses have the same magnitude. Therefore, the horizontal shear stress calculation only requires knowing the transverse shear stress value, as they are both the same.
Image of a rectangular beam subjected to a transverse load.
Rectangular beam under transverse shear VV. τmax\tau_{max} occurs at the horizontal centroidal axis, where QQ is maximum.
  • The shear stress not only varies vertically about the neutral axis but also across the width tt of the beam. Therefore, the shear stress equation and its derivatives also give us a (horizontal) average stress value (τave=VQ/It\tau_\text{ave} = VQ/It). For "short" or "flat" cross-sections, the deviation of the real stress from τave\tau_\text{ave} is high. For example, the maximum and minimum shear stress in rectangular beams (at its center) increase their deviation from τave\tau_\text{ave} as the base-to-height ratio (b/db/d) increases:
































What are the shear stress units?

The shear stress units are pascal (Pa) in the International System of Units and pound per square inch (psi) in the United States customary units system. As stress is usually a big number, other used shear stress units are kPa, MPa, or kpsi.

What is the polar moment of inertia of a circle of 10 cm radius?

The polar moment of inertia of a circle of 10 cm radius is 15708 cm⁴. In the United States customary units system units, the polar moment of inertia is 377.4 in⁴.

How do I calculate the shear stress of a fluid?

To calculate the shear stress 𝜏yx of a fluid:

  1. Determine whether it is a Newtonian or non-Newtonian fluid.
  2. For a Newtonian fluid, multiply the viscosity μ by the shear rate du/dy: 𝜏yx = μ(du/dy).
  3. If it's non-Newtonian, multiply the apparent viscosity η by the shear rate du/dy:
    𝜏yx = η(du/dy).

η and μ are analog terms, with the difference that η varies with du/dy.

How do I calculate viscosity from shear stress and shear rate?

To calculate viscosity μ from shear stress 𝜏yx and shear rate du/dy, divide the shear stress by the shear strain:

μ = 𝜏yx/(du/dy)

How do I calculate shear stress in bolts?

The maximum shear stress of a screw body subjected to torsion is:

𝜏max = 16T/(πdᵣ³)


  • 𝜏max – Maximum nominal shear stress;
  • T – Torque applied to the screw; and
  • d – Minor diameter of the screw.

Load characteristics

arbitrary beam subjected to transverse load

With this option, you calculate the shear stress at a distance y' from the neutral axis (NA) of a beam subjected to a shear force V, using the shear formula 𝜏 = VQ/It.

You can use the section modulus calculator (in its advanced mode) to find the neutral axis and moment of inertia of cross sections, which will help you to find Q.

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