Shaft Torsion Calculator
Calculate torsional shear stress, angle of twist, and polar moment of inertia for shafts.
Torsion Produces Shear Stress and Twist
A torque applied to a circular shaft creates shear stress that increases from zero at the center to a maximum at the outer surface. For elastic Saint-Venant torsion of a circular shaft, τ(r)=Tr/J and θ=TL/(JG). The polar second moment J describes geometric resistance to torsion: J=πd4/32 for a solid circular shaft and π(D4−d4)/32 for a hollow shaft.
The fourth-power dependence makes shaft diameter extremely influential. These formulas are intended for circular shafts in linear elastic torsion; noncircular sections warp and require different torsion constants and stress distributions.
| Symbol | Meaning | Why it appears / units |
|---|---|---|
| T | Applied torque | N·m. |
| J | Polar second moment | m⁴; geometric torsional stiffness term. |
| G | Shear modulus | Pa. |
| c | Outer radius | m; location of maximum shear stress. |
Strength and stiffness are separate checks. A shaft can remain below allowable shear stress yet twist too much for alignment or control requirements. Hollow shafts can be efficient because material far from the center contributes strongly to J.
Torsional shear stress should increase linearly from the center to the outer radius in a circular shaft. The maximum is τmax=Tr/J. Because J depends strongly on diameter, a small diameter change can produce a large change in stress and twist.
Worked Examples
Common Mistakes
Bending uses I; circular-shaft torsion uses J.
J contains length to the fourth power, so unit mistakes can change results by huge factors.
Rectangular and open sections warp and need different torsion constants and stress relations.
Frequently Asked Questions
Formula Explorer connections
Interpretation: This formula is the rotational counterpart of linear mechanics, relating angle, angular motion, torque, inertia or rotational energy. Assumption: Define the rotation axis and sign convention. Rigid-body behavior, no slipping, steady rotation or negligible bearing losses may be assumed.