The formula is given by:
\[
\tau = \frac{T}{J} \cdot r
\]
where \( \tau \) is the shear stress, \( T \) is the torque, \( J \) is the polar moment of inertia, and \( r \) is the radius of the shaft. For a circular shaft, the polar moment of inertia \( J \) is
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