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two samples 1 and 2 are initially kept in the same state. the sample 1 is expanded through an isothermal process where as sample 2 through an adiabatic process up to the same final volume.Let `p_(1)` and `p_(2)` be the final pressure of the samples and 2 respectively in the previous question then.

A

`p_(1)gtp_(2)`

B

`p_(1)=p_(2)`

C

`p_(1)ltp_(2)`

D

The relation between `p_(1)` and `p_(2)` cannot be deduced

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The correct Answer is:
To solve the problem, we need to analyze the behavior of two gas samples undergoing different types of expansion: isothermal for sample 1 and adiabatic for sample 2. We will derive the final pressures \( P_1 \) and \( P_2 \) for both samples and compare them. ### Step-by-Step Solution: 1. **Define Initial Conditions**: - Let the initial pressure and volume for both samples be \( P_0 \) and \( V_0 \) respectively. 2. **Isothermal Process for Sample 1**: - In an isothermal process, the temperature remains constant. According to the ideal gas law, we have: \[ P_1 V_f = P_0 V_0 \] - Rearranging this equation to find the final pressure \( P_1 \): \[ P_1 = \frac{P_0 V_0}{V_f} \] 3. **Adiabatic Process for Sample 2**: - In an adiabatic process, the relationship between pressure and volume is given by: \[ P_2 V_f^\gamma = P_0 V_0^\gamma \] - Rearranging this equation to find the final pressure \( P_2 \): \[ P_2 = \frac{P_0 V_0^\gamma}{V_f^\gamma} \] 4. **Comparison of Final Pressures**: - Now we have: \[ P_1 = \frac{P_0 V_0}{V_f} \] \[ P_2 = \frac{P_0 V_0^\gamma}{V_f^\gamma} \] - To compare \( P_1 \) and \( P_2 \), we can analyze the ratio: \[ \frac{P_1}{P_2} = \frac{\frac{P_0 V_0}{V_f}}{\frac{P_0 V_0^\gamma}{V_f^\gamma}} = \frac{V_f^\gamma}{V_f} \cdot \frac{V_0}{V_0^\gamma} = \frac{V_f^{\gamma - 1}}{V_0^{\gamma - 1}} \] - Since \( \gamma > 1 \) and \( V_f > V_0 \), we know that \( V_0 < V_f \), which implies that \( \frac{V_0}{V_f} < 1 \). Thus, \( P_1 > P_2 \). 5. **Conclusion**: - Therefore, we conclude that: \[ P_1 > P_2 \] - The correct option is (a) \( P_1 \) is greater than \( P_2 \).
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