Stress due to radial temperature gradient in a tube

AI Thread Summary
The discussion focuses on calculating the radial stress gradient in a thick-walled tube due to temperature variations. The stress depends on whether the tube can expand; if constrained, maximum stress is calculated using thermal strain and Hooke's law. However, the tube in question is free to expand, leading to differential expansion between hot and cold walls, resulting in hoop and radial stress. For detailed calculations, Roark's Formulas for Stress & Strain provides relevant equations for maximum stress on surfaces with differing temperatures. The goal is to derive stress as a function of radial position based on the temperature gradient.
StoneME
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Anyone know how to use the temperature gradient in a thick-walled tube to calculate the stress seen throughout the wall (radial stress gradient)? I've been scouring the internet for a good explanation but haven't found one.
 
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The stress will depend on if the tube is allowed to expand or if it can't move when it gets hot.

If it is not allowed to expand, the stress is maximum and is determined as follows:

ΔR = \alpha Ro \Delta T

The thermal strain is now:

\epsilon = ΔR / Ro = \alpha \Delta T

And the stress is figured with Hooke's law:

σ = E \epsilon
 
First, I should be more clear. The tube is not being constrained and is free to expand.

Second, I appreciate the response but I think I'm looking for a little more depth. What I'm looking for is a description of stress as a function of radial position given the temperature as a function of radial position. Temperature gradients will cause the hot wall (inner or outer) to expand more than the cold wall, giving rise to hoop stress as well as radial stress.
 
Roark's Formulas for Stress & Strain, Chapter 16, Section 16.6, Case 16 has formulas for max stress on the surfaces of a hollow cylinder with two different temperatures on the inner and outer surface. They look pretty easy. You may be able to extend this to determine σ(r).
 
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