Mechanics of Materials

Combined Loading Stress Calculator

Stresses at a point under axial, bending, shear and torsion loads, with principal stresses, von Mises and factor of safety.

Tool no.
ECT-S26
Rev
1.0
Updated
Oct 2026
Method
Superposition + stress transformation
How to use this calculator

Choose the cross-section and the point (top, bottom or side), then enter the internal forces and moments at that section from your free-body diagram. Add the yield strength for a factor of safety.

Formulas

Normal stressσ = N/A − Mzy/Iz + Myz/Iy
Shear stressτ = Tc/J + VQ/(It)
Principalσ1,2 = σ/2 ± √((σ/2)² + τ²)
von Misesσ′ = √(σ² + 3τ²)

Worked example

50 mm solid shaft with 20 kN tension, 1.2 kN·m bending and 1.5 kN·m torque, top point (the default)

  1. A = 1963 mm², I = 306 800 mm⁴, J = 613 600 mm⁴.
  2. σ = 20 000/1963 − 1.2×10⁶(25)/306 800 = 10.19 − 97.78 = −87.6 MPa; τ = 1.5×10⁶(25)/613 600 = 61.1 MPa.
  3. σ1,2 = 31.4 and −119.0 MPa; von Mises 137.4 MPa.

Frequently asked questions

Where is the critical point?

Usually on the outer surface where bending stress is largest, but check the neutral axis too when transverse shear is large.

Which failure theory should I use?

von Mises (distortion energy) for ductile metals is the most accurate; Tresca (maximum shear) is slightly more conservative.