Understanding Heat Flow Between Concentric Cylinders

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The discussion focuses on deriving the heat flow expression for concentric cylinders, specifically P = [(2*pi)*L*k*T] / ln(b/a). The user is trying to understand how to adapt the heat flow equation for a slab to this cylindrical geometry, noting that the area A transforms to the cylindrical surface area. There is confusion about integrating from the outer to inner radius and how the variables will interact during this process. The relationship between heat flow and electric flux is mentioned as a potential analogy, but clarity is sought on the integration steps. The conversation also touches on using LaTeX for formatting mathematical equations.
bemigh
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Hey everyone...
I think I am not picking up on something here...
The rate of heat flow across a slab is:
P = (k*A*T)/D
where k is the thermal conductivity of the medium,
A is the cross sectional medium
and T is the temperature difference
and P is power...

Now.. .for my lab, I am using to concentric cylinders...

and I have to derive this expression for the heat flow between two concentric cylinders:
P = [(2*pi)*L*k*T] / ln(b/a)
where L is the length of the cylinders, and b is the radius of the outer cyliner, and a is the radius of the inner cylinder...

Now the lab is saying that the mathematics is essentially the same as for the electric field between two cylinders, and the heat flow is analogous to the electric flux... but i can't see how that helps me...

My thinking is this... the area A becomes the area of a cylinder, 2*pi*r*L, and D becomes r... but how can I possibly integrate from b to a, because now my r's will cancel?? any help is appreciated...
Cheers
 
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I'm assuming you have a constant J.
J = -\kappa A \nabla T
J = -\kappa (2 \pi r L) \frac{\partial T}{\partial r}
\frac{dr}{r} = -\kappa (2 \pi L) dT / J
\ln(b/A) = -\kappa (2 \pi L) \Delta T / J
J = -\kappa (2 \pi L) \Delta T / \ln(b/A)
 
thanks a lot for your help,
PS, how do i type that script you use for your reply?
 
Last edited:

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