Two identical plates $ P $ and $ Q $, radiating as perfect black bodies, are kept in vacuum at constant absolute temperatures $ T_P $ and $ T_Q $, respectively, with $ T_Q<T_P $, as shown in Fig. 1. The radiated power transferred per unit area from $ P $ to $ Q $ is $ W_0 $. Subsequently, two more plates, identical to $ P $ and $ Q $, are introduced between $ P $ and $ Q $, as shown in Fig. 2. Assume that heat transfer takes place only between adjacent plates. If the power transferred per unit area in the direction from $ P $ to $ Q $ (Fig. 2) in the steady state is $ W_S $, then the ratio $ \dfrac{W_0}{W_S} $ is ____. 
Step 1: Power radiated between two black bodies
For two black bodies at temperatures \( T_P \) and \( T_Q \), the net power radiated per unit area is given by the Stefan-Boltzmann law:
\[ W = \sigma \left( T_P^4 - T_Q^4 \right) \]
So initially (Fig. 1), the power is:
\[ W_0 = \sigma \left( T_P^4 - T_Q^4 \right) \]
Step 2: Insert two intermediate black plates
In Fig. 2, two additional identical black plates are placed between \( P \) and \( Q \). Let the four plates be \( P, A, B, Q \) from left to right.
Assume steady state and let the temperatures of the intermediate plates be \( T_1 \) and \( T_2 \), such that:
\[ T_P>T_1>T_2>T_Q \]
Now, energy is transferred between adjacent pairs only:
At steady state, the energy flow rate must be the same through all three segments:
\[ \sigma (T_P^4 - T_1^4) = \sigma (T_1^4 - T_2^4) = \sigma (T_2^4 - T_Q^4) \]
Let this common value be \( W_S \), then:
\[ T_P^4 - T_1^4 = T_1^4 - T_2^4 = T_2^4 - T_Q^4 = \Delta \]
Therefore:
\[ \begin{align} T_P^4 - T_Q^4 &= (T_P^4 - T_1^4) + (T_1^4 - T_2^4) + (T_2^4 - T_Q^4) \\ &= 3\Delta = \frac{3W_S}{\sigma} \Rightarrow W_S = \dfrac{1}{3} \sigma (T_P^4 - T_Q^4) \end{align} \]
Step 3: Compute the ratio
\[ \frac{W_0}{W_S} = \frac{\sigma (T_P^4 - T_Q^4)}{(1/3) \sigma (T_P^4 - T_Q^4)} = \boxed{3} \]



| List-I | List-II | ||
| P | Work done in the complete cyclic process | I | \(ℛT_0 − 4ℛT_0 ln 2\) |
| Q | Change in the internal energy of the gas in the process JK | II | \(0\) |
| R | Heat given to the gas in the process KL | III | \(3ℛT_0\) |
| S | Change in the internal energy of the gas in the process MJ | IV | \(−2ℛT_0 ln 2\) |
| \[−3ℛT_0 ln 2\] | |||
An ideal monatomic gas of $ n $ moles is taken through a cycle $ WXYZW $ consisting of consecutive adiabatic and isobaric quasi-static processes, as shown in the schematic $ V-T $ diagram. The volume of the gas at $ W, X $ and $ Y $ points are, $ 64 \, \text{cm}^3 $, $ 125 \, \text{cm}^3 $ and $ 250 \, \text{cm}^3 $, respectively. If the absolute temperature of the gas $ T_W $ at the point $ W $ is such that $ n R T_W = 1 \, J $ ($ R $ is the universal gas constant), then the amount of heat absorbed (in J) by the gas along the path $ XY $ is 