HEAT TRANSFER IN A CONDUCTING BAR

An electric current I flows along homogenous conducting bar with length L resistivity R and thermal conductivity K . The two ends are located at X=0 and X=L In the OX axis .The temperature X=0 is T=T1 and X=L is T=T2(T1>T2) both temperatures are kept constant. USE FOURIER LAW FOR HEAT TRANSFER AND CONSIDER ONLY JOULE LAW FOR HEAT DISSAPATION IF T1=500k , T2=200K , Crossectional area S=1 m^2 , K=109 SI unit ,L=2m,R=9.71,I=3 FIND temperature of mid point of rod


The answer is 350.4.

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1 solution

Karan Chatrath
May 23, 2020

Very nice problem. As current flows through the slab, the heat generated per unit time in the whole volume of the slab is:

P = R L S I 2 P = \frac{RL}{S}I^2

Therefore, the power generated per unit time, per unit volume is:

p = P L S p = \frac{P}{LS}

Now, consider an elementary volume of cross-section area S S and length δ x \delta x at a distance x x from the left end of the slab. The hear generated per unit time in this elementary volume is:

P v = p S δ x P_v = p S \ \delta x

Now, consider this elementary volume again. The heat per unit time flowing into the left facet of this element is Q i n Q_{in} and heat per unit time flowing out of this slab through its right facet is Q o u t Q_{out} . Applying the first law of thermodynamics for this elementary volume gives:

Q i n + P v = Q o u t ( 1 ) Q_{in} + P_v = Q_{out} \ \dots (1)

Now, the rate of hear flow varies with x x . Since δ x \delta x is small, one can use a Taylor series first order approximation (since δ x \delta x is small) to relate Q i n Q_{in} and Q o u t Q_{out} as such:

Q o u t = Q i n + d Q i n d x δ x Q_{out} = Q_{in} + \frac{dQ_{in}}{dx}\delta x Q o u t Q i n = d Q i n d x δ x \implies Q_{out} - Q_{in} = \frac{dQ_{in}}{dx}\delta x

Now, using Fourier's law, we know that:

Q i n = K S d T d x Q_{in} = -KS \frac{dT}{dx} d Q i n d x = K S d 2 T d x 2 \implies \frac{dQ_{in}}{dx} = -KS \frac{d^2T}{dx^2} Q o u t Q i n = K S d 2 T d x 2 δ x \implies Q_{out} - Q_{in} = -KS \frac{d^2T}{dx^2} \delta x

Substituting the above result in (1) gives:

P v = K S d 2 T d x 2 P_v = -KS \frac{d^2T}{dx^2} d 2 T d x 2 = R I 2 K S 2 \implies \boxed{\frac{d^2T}{dx^2}=-\frac{RI^2}{KS^2}}

We know that T ( 0 ) = T 1 T(0) = T_1 and T ( L ) = T 2 T(L) = T_2 .

Double integrating the above equation and substituting all boundary conditions and values gives the temperature distribution as a function of x x as follows. Simplifications have been left out in this solution.

T ( x ) = 8739 x 2 21800 1626261 x 10900 + 500 T(x) = -\frac{8739\,x^2}{21800}-\frac{1626261\,x}{10900}+500

From the above equation, T ( L / 2 ) T(L/2) can be conveniently computed. The result is T ( L / 2 ) 350.4 K \boxed{T(L/2) \approx 350.4 \ K} .

Nice one mate!

Krishna Karthik - 1 year ago

@Karan Chatrath good solution please post more mechanics questions

DARK ANGEL - 1 year ago

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