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A Carnot's engine is made to work betwee...

A Carnot's engine is made to work between `200^(@)C` and `0^(@)C` first and then between `0^(@)C` and `-200^(@)C`. The ratio of efficiencies of the engine in the two cases is

A

`1.73 : 1`

B

`1 : 1.73`

C

`1 : 1`

D

`1 : 2`

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To find the ratio of efficiencies of a Carnot engine working between two different temperature ranges, we can follow these steps: ### Step 1: Understand the formula for efficiency of a Carnot engine The efficiency (\( \eta \)) of a Carnot engine is given by the formula: \[ \eta = 1 - \frac{T_C}{T_H} \] where \( T_C \) is the absolute temperature of the cold reservoir and \( T_H \) is the absolute temperature of the hot reservoir. ### Step 2: Convert temperatures to Kelvin For the first case, the temperatures are: - Hot reservoir (\( T_H \)) = \( 200^\circ C = 200 + 273 = 473 \, K \) - Cold reservoir (\( T_C \)) = \( 0^\circ C = 0 + 273 = 273 \, K \) For the second case, the temperatures are: - Hot reservoir (\( T_H \)) = \( 0^\circ C = 273 \, K \) - Cold reservoir (\( T_C \)) = \( -200^\circ C = -200 + 273 = 73 \, K \) ### Step 3: Calculate efficiencies for both cases **Efficiency for the first case (\( \eta_1 \))**: \[ \eta_1 = 1 - \frac{T_C}{T_H} = 1 - \frac{273}{473} = 1 - 0.577 = 0.423 \] **Efficiency for the second case (\( \eta_2 \))**: \[ \eta_2 = 1 - \frac{T_C}{T_H} = 1 - \frac{73}{273} = 1 - 0.267 = 0.733 \] ### Step 4: Calculate the ratio of efficiencies Now, we find the ratio of the efficiencies: \[ \frac{\eta_1}{\eta_2} = \frac{0.423}{0.733} \] Calculating this gives: \[ \frac{\eta_1}{\eta_2} \approx 0.577 \] ### Step 5: Finalize the answer The ratio of efficiencies of the engine in the two cases is approximately: \[ \frac{\eta_1}{\eta_2} \approx 0.577 \]

To find the ratio of efficiencies of a Carnot engine working between two different temperature ranges, we can follow these steps: ### Step 1: Understand the formula for efficiency of a Carnot engine The efficiency (\( \eta \)) of a Carnot engine is given by the formula: \[ \eta = 1 - \frac{T_C}{T_H} \] where \( T_C \) is the absolute temperature of the cold reservoir and \( T_H \) is the absolute temperature of the hot reservoir. ...
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A2Z-KINETIC THEORY OF GASES AND THERMODYNAMICS-Second Law Of Thermodynamics
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