Heat transfer through a cylindrical shell

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Homework Help Overview

The problem involves heat transfer through an infinitely long cylindrical shell with specified inner and outer radii, temperatures, and thermal conductivity. The original poster attempts to determine the rate of heat flow per unit length between the inner and outer surfaces.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • Participants discuss the application of a formula intended for flat surfaces to a cylindrical geometry, questioning the appropriateness of the original poster's approach. There is also a focus on the need to consider the geometry of the problem, particularly regarding the cross-sectional area for heat transfer.

Discussion Status

Participants are exploring different interpretations of the heat transfer problem, with some suggesting the need to solve the Laplace equation for the cylindrical geometry. There is no explicit consensus, but guidance is being offered regarding the limitations of the original formula and the necessity of adapting to the cylindrical coordinates.

Contextual Notes

There is a noted concern regarding the applicability of certain equations to the geometry of the problem, with specific emphasis on the assumption of a thin shell and the implications for the heat transfer analysis.

Ian Baughman
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Homework Statement


An infinitely long cylindrical shell has an inner radius a and outer radius b. If the inside is maintained at a temperature Ta and the outside at a temperature Tb, determine the rate of heat flow per unit length between inner and outer surfaces assuming the shell has a thermal conductivity k.

Homework Equations


[/B]
H = -KA((TH-TC)/L)

The Attempt at a Solution


[/B]
1) I said let TH = Ta and TC = Tb
2) I let L = b-a so my new expression is:
H = -KA((Ta-Tb)/(b-a))​
3) My issue here is I can not figure out what to use for the cross sectional area A. In the example I was using as reference the heat was flowing through the pipe not the outer shell of it so the cross sectional area was easy to calculate.
4) My idea was to use 2πr and multiply it by the length of the shell but since it is an infinitely long cylindrical shell that wouldn't make sense to do.
 
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Your formula is only applicable to heat transfer through a flat surface. To find the stationary state in a different geometry you have to solve the Laplace equation for that geometry.

Also note that you are asked for the transfer per unit length of the cylinder.
 
Orodruin said:
Your formula is only applicable to heat transfer through a flat surface. To find the stationary state in a different geometry you have to solve the Laplace equation for that geometry.

Also note that you are asked for the transfer per unit length of the cylinder.
Do you mean like starting with the definition of heat transfer, H = (dQ/dT) or H = -KA(dT/dx), and solving from there using Laplace?
 
Ian Baughman said:
Do you mean like starting with the definition of heat transfer, H = (dQ/dT) or H = -KA(dT/dx), and solving from there using Laplace?
That differential equation is only valid for heat transfer in one dimension (flat geometry). You cannot apply it here unless your shell is very thin. In general you need to solve the heat equation in cylinder coordinates - which for a stationary situation is equivalent to laplace equation.
 

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