ShaftStresses:
% Computes shaft stresses.
Type ShaftStresses for a demo.
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Form:
[tau, alpha, j] = ShaftStresses( t, rI, rO, l, g )
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Inputs
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t (1,1) Torque (Nm)
rO (1,1) Outer radius (m)
rI (1,1) Inner radius (m)
l (1,:) Length (m)
g (1,1) Modulus of rigidity (Pa)
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Outputs
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tau (1,1) Torsional stress (Pa)
alpha (1,1) Twist angle
j (1,1) Moment of inertia (m^4)
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Reference: J. Dugundji, "16.20 Structural Mechanics Course Notes,"
MIT, 1976.
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