1. | \(\text{If}~P_1>P_2~\text{then}~T_1<T_2\) |
2. | \(\text{If}~V_2>V_1~\text{then}~T_2>T_1\) |
3. | \(\text{If}~V_2>V_1~\text{then}~T_2<T_1\) |
4. | \(\text{If}~P_1>P_2~\text{then}~V_1>V_2\) |
A gas undergoes an isothermal process. The specific heat capacity of the gas in the process is:
1. | infinity | 2. | \(0.5\) |
3. | zero | 4. | \(1\) |
1. | \(4\) | 2. | \(1\) |
3. | \(2\) | 4. | \(3\) |
A. | Pressure | B. | Total heat |
C. | Temperature | D. | Volume |
E. | Work done |
1. | A, B and E only | 2. | B, C and D only |
3. | A, B and C only | 4. | A, C and D only |
One mole of an ideal gas at an initial temperature of \(T\) K does \(6R\) joules of work adiabatically. If the ratio of specific heats of this gas at constant pressure and at constant volume is \(5/3\), the final temperature of the gas will be:
1. \((T-2.4)\) K
2. \((T+4)\) K
3. \((T-4)\) K
4. \((T+2.4)\) K
The initial pressure and volume of a gas are P and V respectively. First, its volume is expanded to 4V by an isothermal process and then compressed adiabatically to volume V. The final pressure will be (γ = 1.5):
1. | 8P | 2. | 4P |
3. | P | 4. | 2P |
1. | \(\Delta {U}=-{W}\) in an isothermal process. |
2. | \(\Delta {U}={W}\) in an isothermal process. |
3. | \(\Delta {U}=-{W}\) in an adiabatic process. |
4. | \(\Delta {U}={W}\) in an adiabatic process. |