
1. Process from A to B (Adiabatic Compression):
For the adiabatic compression process \( A \rightarrow B \), the work done can be calculated using the formula for adiabatic processes:
\[ W_{\text{A to B}} = \frac{P_B V_B - P_A V_A}{1 - \gamma} \] where \( P_A \) and \( V_A \) are the pressure and volume at state A, \( P_B \) and \( V_B \) are the pressure and volume at state B, and \( \gamma = \frac{5}{3} \) is the adiabatic index for a monoatomic gas. From the given graph, the volume at state A and state B can be determined, and the corresponding pressures are given in the diagram. We can substitute these values to calculate the work done in this process. This process involves compression, so work will be done on the gas, which will be negative.
2. Process from B to C (Isothermal Expansion):
For the isothermal expansion process \( B \rightarrow C \), the work done by the gas is calculated using the formula for isothermal processes:
\[ W_{\text{B to C}} = nRT \ln \frac{V_C}{V_B} \] where \( n \) is the number of moles of gas, \( R \) is the universal gas constant, \( T \) is the temperature (which remains constant for an isothermal process), \( V_B \) is the volume at state B, and \( V_C \) is the volume at state C. Using the ideal gas law \( PV = nRT \), we can find the work done by the gas as it expands from state B to C. Since the gas is expanding, the work done will be positive.
3. Process from C to A (Isobaric Process):
For the process \( C \rightarrow A \), since the temperature remains constant, the work done in this process is zero because there is no volume change during an isobaric process where the temperature remains constant.
4. Final Calculations:
By substituting the values from the graph into these equations, we calculate the total work done and determine the magnitudes for each process:
Final Answer:
The correct options are B, C, D.


| 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 | \(−2ℛT_0 ln 2\) |
| \[−3ℛT_0 ln 2\] | |||
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 ____. 
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 
Thermodynamics in physics is a branch that deals with heat, work and temperature, and their relation to energy, radiation and physical properties of matter.
A thermodynamic system is a specific portion of matter with a definite boundary on which our attention is focused. The system boundary may be real or imaginary, fixed or deformable.
There are three types of systems:
A system undergoes a thermodynamic process when there is some energetic change within the system that is associated with changes in pressure, volume and internal energy.
There are four types of thermodynamic process that have their unique properties, and they are:
The Zeroth law of thermodynamics states that if two bodies are individually in equilibrium with a separate third body, then the first two bodies are also in thermal equilibrium with each other.
The First law of thermodynamics is a version of the law of conservation of energy, adapted for thermodynamic processes, distinguishing three kinds of transfer of energy, as heat, as thermodynamic work, and as energy associated with matter transfer, and relating them to a function of a body's state, called internal energy.
The Second law of thermodynamics is a physical law of thermodynamics about heat and loss in its conversion.
Third law of thermodynamics states, regarding the properties of closed systems in thermodynamic equilibrium: The entropy of a system approaches a constant value when its temperature approaches absolute zero.