Elastic energy stored in a shaft under torsion?

AI Thread Summary
The discussion focuses on calculating the elastic energy stored in a hollow drive shaft subjected to a constant torque. Key equations include the relationship between torque, shear stress, and the shear modulus, as well as the formula for elastic energy per unit volume. The user attempts to derive the total elastic energy and expresses concern about the high power of the outer radius in their result. They seek clarification on the factor of 1/2 in the work done equation, which is explained through the area of a triangle on a T-θ diagram. The conversation emphasizes the importance of using the correct modulus and understanding the relationship between torque and angular displacement.
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Homework Statement


Consider a hollow drive shaft of length L, inner radius b, outer radius a. A constant torque is applied (we can assume one end of the shaft is fixed because we're applying a constant torque T regardless of the angular velocity of the shaft). We know material properties of the shaft, G the shear modulus and E young's modulus, plus any others we might need.

Homework Equations


(i) T/K = G\Theta/L = \tau/r
(ii) K for a hollow cylinder is K = (\pi/2)(a^{4} - b^{4})
(iii) Elastic energy stored per unit volume P = (1/2)(\sigma^{2}/E) where \sigma is the maximum stress applied to that unit area

The Attempt at a Solution


I'm not sure if these are all the relevant equations, but here is what I've tried.
- At any point distance r from the center of the cylinder, there is a shear stress \tau = rT/K = (rT\pi/2)(a^{4} - b^{4}). If I plug this into my original equation for elastic energy per unit volume, then integrate over the volume of the cylinder, I find

E(T) = 1/(2E)\int\int\int[(\pirT/2)(a^{4} - b^{4})]^2 dr d\theta dL.

I get as a result

E(T) = ((\pi^{3}LT^{2})/(12E)) (a^{4} - b^{4})^{2} (a^{3} - b^{3}))

This answer seems fairly reasonable, because it depends on L, but I am a little worried that it would have a factor of a^8, which seems excessively high for an engineering problem. Also, I'm skeptical of being able to substitute shear stress from (i) for tensile stress in (iii). Would I use the shear modulus G instead of young's modulus E? Is this derivation mostly correct, or is there a complete different approach?
 
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The work done is given by Uk=Tθ/2.

From the equation of three above you can find θ in terms of T and find Uk.
 
I understand the idea behind Uk=Tθ/2, but where does the factor of 1/2 come from?

From what I understand, the work done by a torque over an angular distance is given by \int Td\theta, integrated from 0 to \theta, which results in an equation for the energy put into the shaft being:
U_{k} = T \theta

Using your method, I come to the following solution:
\theta=LT/KG
K = (\pi/2)(a^{4} - b^{4}), L, T and G are constants

then U_{k} = (LT^{2})/((G\pi/2)(a^{4} - b^{4})), or 1/2 that using your equation of U_{k} = T\theta/2

This answer is definitely more accurate. I realize that since rotation is linearly related to torque and elastic energy is stored as the square of the angular rotation, T should be squared as the new equation.

If possible, help me understand the factor of 2 please.
 
Torque relates linearly with angle θ.

So on a T-θ diagram, from 0 to θ, the shape (graph) formed is a triangle of height T and base θ.

The area under that graph gives the work done Uk. So Uk=(T)*(θ)/2=Tθ/2
 
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