Minimum Principal Stress (Mohr's Circle)

Also known as minimum principal stress · sigma 2 plane stress · minor principal stress · Mohr's circle second principal stress · plane stress transformation

σ2=σx+σy2(σxσy2)2+τxy2\sigma_2 = \frac{\sigma_x + \sigma_y}{2} - \sqrt{\left(\frac{\sigma_x - \sigma_y}{2}\right)^{2} + \tau_{xy}^{2}}

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The minor principal stress is the other end of the same diameter: centre minus radius. For σx=100\sigma_x = 100, σy=40\sigma_y = 40, τxy=40\tau_{xy} = 40 MPa the centre is 70 and the radius 50, so σ1=120\sigma_1 = 120 and σ2=20\sigma_2 = 20 MPa. Verify with the product invariant: 120×20=2400120 \times 20 = 2400, and σxσyτxy2=40001600=2400\sigma_x\sigma_y - \tau_{xy}^2 = 4000 - 1600 = 2400. The two principal planes are always exactly 90° apart, which is the one geometric fact about Mohr's circle worth memorising.

σ2\sigma_2 is the stress people neglect and then regret. In a pressure vessel it is the longitudinal stress, half the hoop; in a rolling contact it is a large compression that makes the shear beneath the surface, not at it, the place fatigue cracks start. And when σ2\sigma_2 goes negative while σ1\sigma_1 stays positive, the circle straddles the origin and the element is in the state closest to pure shear — the worst case for a ductile material, because the maximum shear is then (σ1σ2)/2(\sigma_1 - \sigma_2)/2, larger than either principal stress on its own.

The classic mistake is treating σ2\sigma_2 as unimportant because it is smaller. For cast iron, concrete and other brittle materials the governing check is σ1\sigma_1 against tensile strength — but for steel every yield criterion in use, Tresca and von Mises alike, is built from the difference between principal stresses, so σ2\sigma_2 is half the answer. A biaxial tension state with σ1=σ2\sigma_1 = \sigma_2 has zero in-plane shear and will not yield at all under Tresca, which is why a spherical pressure vessel is the most efficient shape there is.

Minimum Principal Stress (Mohr's Circle)
σ2=σx+σy2(σxσy2)2+τxy2\sigma_2 = \frac{\sigma_x + \sigma_y}{2} - \sqrt{\left(\frac{\sigma_x - \sigma_y}{2}\right)^{2} + \tau_{xy}^{2}}
Where
  • σ2\sigma_2= Minimum principal stress (kPa)
  • σx\sigma_x= Normal stress on the x face (kPa)
  • σy\sigma_y= Normal stress on the y face (kPa)
  • τxy\tau_{xy}= Shear stress on the element (kPa)
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