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According to the maximum normal stress theory, the diameter of circular shaft subjected to bending moment M and torque T is (where σy is the yield stress in the uniaxial tensile test and N is the factor of safety)

A[Nπσy(16M+16M2+T2)]12[\frac{N}{\pi \sigma_y}(16M+16\sqrt{M^2+T^2})]^{\frac 12}

B[1πNσy(16M+16M2+T2)]12[\frac{1}{\pi N \sigma_y}(16M+16\sqrt{M^2+T^2})]^{\frac 12}

C[1πNσy(16M+16M2+T2)]13[\frac{1}{\pi N \sigma_y}(16M+16\sqrt{M^2+T^2})]^{\frac 13}

D[Nπσy(16M+16M2+T2)]13[\frac{N}{\pi \sigma_y}(16M+16\sqrt{M^2+T^2})]^{\frac 13}

Answer:

[Nπσy(16M+16M2+T2)]13[\frac{N}{\pi \sigma_y}(16M+16\sqrt{M^2+T^2})]^{\frac 13}

Read Explanation:

The maximum normal stress theory states that for no failure, the maximum principal stress should be less than the yield stress under uniaxial loading. The diameter of a circular shaft subjected to bending moment M and torque T is given by d=[Nπσy(16M+16M2+T2)]13d = [\frac{N}{\pi \sigma_y}(16M+16\sqrt{M^2+T^2})]^{\frac 13} , where N is the factor 1 of safety, ay is the yield stress in uniaxial tensile test. This is derived using the formula for combined effect of bending and torsion, and the expression for maximum principal stress.


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