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Question: A partition wall is made of two layers of different materials, A and B, in contact with each other. ...

A partition wall is made of two layers of different materials, A and B, in contact with each other. Both A and B have the same thickness but, the thermal conductivity of layer A is twice that of layer B. At steady state, if the temperature difference across the layer B is 50K, then find the corresponding difference across the layer A.
A) 50K
B) 12.5K
C) 25K
D) 60K
E) 6025K

Explanation

Solution

At steady state, the rate of heat flow (also known as heat current) dQdt\dfrac{{dQ}}{{dt}} for both the layers A and B will be the same, i.e., dQAdt=dQBdt\dfrac{{d{Q_A}}}{{dt}} = \dfrac{{d{Q_B}}}{{dt}} and it depends on the thermal conductivity of the layer, is proportional to the temperature difference between the junction and layer and is inversely proportional to the distance between then (thickness of the layer).

Formula used:
The rate of heat flow is given by, dQdt=κAdTd\dfrac{{dQ}}{{dt}} = \kappa A\dfrac{{dT}}{d}, where κ\kappa is the thermal conductivity of the layer, AA is the area of the layer, dTdT is the temperature difference between two endpoints, dd is the thickness of the layer.

Complete step by step solution:
Step 1: Sketch a rough diagram of the problem.

Step 2: List the information given in the question.
Let the temperature at the junction be TT.
Let the temperature difference across layer A be dT=TATdT = {T_A} - T and it is unknown.
Let the temperature difference across layer B be dT=TTB=50KdT = T - {T_B} = 50{\text{K}} .
Let thermal conductivity of B be κB=κ{\kappa _B} = \kappa , then that of A will be κA=2κB=2κ{\kappa _A} = 2{\kappa _B} = 2\kappa .
Given, A and B have the same thickness, i.e., dA=dB=d{d_A} = {d_B} = d.
Also, A and B have the same area, i.e., AA=AB=A{A_A} = {A_B} = A.
Step 3: Express the heat flow equation for A and B at a steady-state to find TAT{T_A} - T.
When a steady state has reached the rate of heat flow will be constant across the layers.
Thus, we have dQAdt=dQBdt\dfrac{{d{Q_A}}}{{dt}} = \dfrac{{d{Q_B}}}{{dt}} where dQAdt\dfrac{{d{Q_A}}}{{dt}} represent rate of heat flow through A and dQBdt\dfrac{{d{Q_B}}}{{dt}} represents rate of heat flow through B.
Rate of heat flow through A is given as, dQAdt=2κ(TATd)A\dfrac{{d{Q_A}}}{{dt}} = 2\kappa \left( {\dfrac{{{T_A} - T}}{d}} \right)A .
Rate of heat flow through A is given as, dQBdt=κ(TTBd)A\dfrac{{d{Q_B}}}{{dt}} = \kappa \left( {\dfrac{{T - {T_B}}}{d}} \right)A .
At steady state, 2κ(TATd)A=κ(TTBd)A2\kappa \left( {\dfrac{{{T_A} - T}}{d}} \right)A = \kappa \left( {\dfrac{{T - {T_B}}}{d}} \right)A .
Cancel out similar terms to obtain a simplified form of the above equation.
Now, 2(TAT)=TTB2\left( {{T_A} - T} \right) = T - {T_B} .
Substitute value for TTB=50KT - {T_B} = 50{\text{K}} in the above equation to get required temperature difference, TAT{T_A} - T .
i.e., 2(TAT)=50K2\left( {{T_A} - T} \right) = 50{\text{K}} or TAT=25K{T_A} - T = 25{\text{K}} .
Hence, at a steady-state, the temperature difference across layer A is 25K.

Therefore, the correct option is (C) 25K.

Note:
The junction of the two layers is the endpoint of heat flow for layer A while, it is the start of heat flow for layer B. The temperature difference across each layer must be expressed accordingly.