Designing a Shaft for Specific Torsional Loads

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Designing a shaft for specific torsional loads requires calculating the diameter based on maximum shear stress and material properties. The maximum shear stress can be derived from the yield stress, typically approximated as 0.6 times the tensile yield stress for steel. With a safety factor of 2, the allowable shear stress becomes 0.3 times the tensile yield stress, ensuring the design avoids plastic deformation. The confusion arises from needing a proof for shear stress calculations, which can be supported by the distortion energy theorem. Ultimately, referencing the Steel Code can provide the necessary justification for the shear stress value used in the design.
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I need to design a shaft that have a specific torsional load acting on it. I have the safety factor of 2 and have a table of material properties (yield stress, ultimate stress, shear modulus, modulus of elasticity etc.).

I need to find the diameter of the shaft that resist the specifies torque. I have the formulas of \taumax=Tc/J and angle of twist formula. As the angle of twist formula is related to the length its useless because I don't have any specified. I need to get a \taumax by using material properties but I couldn't find anything to relate them up to now. I have searched many shaft design documents but no results and also I am confused right now.
 
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Now I can make a proof for shear stress with max distortion energy theorem. So I am going to get a yield shear stress from the theorem and using it with factor of safety I will get my desired \taumax to use it in torsion formula, with using the yield stress to find diameter, I will get a diameter free of plastic deformation. Am I right with that?
 
I don't know why you need a proof for shear stress when it's max value can be looked up in a table of material properties. For steel, it's about 0.6 Fy, where Fy is the tensile yield stress. So with a SF of 2, allowable shear stress would be about 0.3Fy and you needn't worry about plastic deformation.
 
The proof is my biggest problem with my work, Because it must be a project style showing how can I derived this 0.6Fy. I need a source to show it.
 
The Steel Code I use calculates the ultimate shear stress as the tensile yield stress divided by square root of 3, which rounds to 0.6 Fy. I do not know if that value comes from the distortion energy theorem to which you refer.
 
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