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Question: Two large black plane surfaces are maintained at constant temperature $T_1$ and $T_2 (T_1 > T_2)$. T...

Two large black plane surfaces are maintained at constant temperature T1T_1 and T2(T1>T2)T_2 (T_1 > T_2). Two thin black plates are placed between the two surfaces and in parallel to these. After some time, steady conditions are obtained. What is the ratio of heat transfer rate between plate-1 & plate-3 to the ratio of original (when plate-3 & plate-4 was not present) heat tranfer rate between plate-1 & plate-2 (η\eta) in steady state?

A

η=12\eta = \frac{1}{2}

B

η=13\eta = \frac{1}{3}

C

η=1\eta = 1

D

η=0\eta = 0

Answer

η=13\eta = \frac{1}{3}

Explanation

Solution

Let AA be the area of the plates and σ\sigma be the Stefan-Boltzmann constant. All surfaces are black bodies, so their emissivity e=1e=1.

Original Situation: The original heat transfer rate per unit area between plate-1 and plate-2 is given by Stefan-Boltzmann's law: Horig=σ(T14T24)H_{orig} = \sigma (T_1^4 - T_2^4)

New Situation: Two thin black plates (plate-3 and plate-4) are placed between plate-1 and plate-2. The arrangement is plate-1, plate-3, plate-4, plate-2. Let their temperatures in steady state be T1,T3,T4,T2T_1, T_3, T_4, T_2 respectively. Since T1>T2T_1 > T_2, it follows that T1>T3>T4>T2T_1 > T_3 > T_4 > T_2 in steady state.

In steady state, the net heat transfer rate per unit area between any two adjacent plates is the same. Let this rate be HnewH_{new}. The heat transfer rate per unit area from plate-1 to plate-3 is: Hnew=σ(T14T34)H_{new} = \sigma (T_1^4 - T_3^4) (1)

The heat transfer rate per unit area from plate-3 to plate-4 is: Hnew=σ(T34T44)H_{new} = \sigma (T_3^4 - T_4^4) (2)

The heat transfer rate per unit area from plate-4 to plate-2 is: Hnew=σ(T44T24)H_{new} = \sigma (T_4^4 - T_2^4) (3)

Adding equations (1), (2), and (3): Hnew+Hnew+Hnew=σ(T14T34)+σ(T34T44)+σ(T44T24)H_{new} + H_{new} + H_{new} = \sigma (T_1^4 - T_3^4) + \sigma (T_3^4 - T_4^4) + \sigma (T_4^4 - T_2^4) 3Hnew=σ(T14T24)3H_{new} = \sigma (T_1^4 - T_2^4)

Comparing this with the original heat transfer rate: 3Hnew=Horig3H_{new} = H_{orig} So, Hnew=Horig3H_{new} = \frac{H_{orig}}{3}

The question asks for the ratio η\eta of the heat transfer rate between plate-1 & plate-3 to the original heat transfer rate between plate-1 & plate-2. The heat transfer rate between plate-1 and plate-3 in the new configuration is HnewH_{new}. The original heat transfer rate between plate-1 and plate-2 is HorigH_{orig}.

Therefore, the ratio η\eta is: η=Heat transfer rate between plate-1 & plate-3Original heat transfer rate between plate-1 & plate-2=HnewHorig\eta = \frac{\text{Heat transfer rate between plate-1 \& plate-3}}{\text{Original heat transfer rate between plate-1 \& plate-2}} = \frac{H_{new}}{H_{orig}}

Substituting Hnew=Horig3H_{new} = \frac{H_{orig}}{3}: η=Horig/3Horig=13\eta = \frac{H_{orig}/3}{H_{orig}} = \frac{1}{3}