Principal Stress Calculator

Find principal stresses, maximum shear stress and principal angle for plane stress.

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Find principal stresses, maximum shear stress and principal angle for plane stress.

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Major principal stress σ₁ (MPa)

Major principal stress σ₁ (MPa)
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Minor principal stress σ₂ (MPa)
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Maximum shear stress (MPa)
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Average normal stress (MPa)
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Principal angle θp (degrees)
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How to use this tool

1
Enter σx and σy

Normal stresses on the x and y faces, in megapascals; tensile is positive.

2
Enter shear stress τxy

Shear stress on the same element, in megapascals.

3
Read principal stresses

These are the maximum and minimum normal stresses, acting on planes with zero shear.

4
Use the principal angle

The rotation to the principal planes, measured from the x-axis.

Formula & worked example

σ₁,₂ = (σx + σy)/2 ± sqrt(((σx − σy)/2)² + τxy²). Maximum shear stress τ_max = sqrt(((σx − σy)/2)² + τxy²). Principal angle θp = ½ × arctan(2τxy / (σx − σy)).

σx = 100, σy = 50, τxy = 30 MPa: average 75 MPa, radius 39.051 MPa, σ₁ = 114.051 MPa, σ₂ = 35.949 MPa, τ_max = 39.051 MPa, θp = 25.097°.

Limitations — read this before you rely on it

This is plane stress (a thin element with zero out-of-plane stress). Full three-dimensional stress states need the third principal stress, and failure prediction additionally requires a material criterion such as von Mises or Tresca.

Frequently asked questions

The extreme normal stresses at a point, acting on planes where shear stress vanishes.

On Mohr’s circle the radius is exactly the largest shear stress, reached on planes at 45° to the principal planes.

Tensile normal stress is positive and compressive negative; shear sign follows the standard element convention.

Then σx and σy are already the principal stresses and the principal angle is zero.

Compare the principal stresses against a yield criterion for your material; this tool reports stresses only, not a pass or fail.