Step 1: Understanding the Question:
The question asks for the state of stress at any point on the outer surface of a circular shaft when it is subjected to a pure twisting moment (pure torsion).
Step 2: Key Formula or Approach:
According to the torsion equation for a circular shaft:
\[ \frac{T}{J} = \frac{\tau}{r} = \frac{G \theta}{L} \]
where:
$T$ is the applied torque.
$J$ is the polar moment of inertia.
$\tau$ is the shear stress at radius $r$.
Step 3: Detailed Explanation:
• Under pure torsion, the only load applied to the shaft is a torque acting about its longitudinal axis.
• There are no axial loads, bending moments, or external pressures acting on the shaft.
• Consequently, the normal stress ($\sigma$) along the longitudinal, radial, and circumferential directions of the shaft is zero ($\sigma = 0$).
• The applied torque produces a shear stress ($\tau$) on planes parallel and perpendicular to the longitudinal axis of the shaft.
• This shear stress is maximum at the outer surface ($r = R$) and varies linearly to zero at the central axis.
• Thus, relative to the coordinate system aligned with the axis of the shaft, the stress state consists entirely of pure shear stress.
Step 4: Final Answer:
The state of stress at any point on the surface of the shaft consists of pure shear stress.