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Concepts Of Physics MCQ Edition [Volume 2]
Exam
Concepts Of Physics MCQ Edition [Volume 2]
Subject
Physics
Chapter
Specific Heat Capacities of Gases

Concepts Of Physics MCQ Edition [Volume 2] · Physics · Specific Heat Capacities of Gases

Two rigid vessels A and B , each having a volume of 200 cm^3 ,...

Two rigid vessels AA and BB, each having a volume of 200 cm3200 \text{ cm}^3, contain an ideal gas (CV=12.5 J K−1 mol−1C_V = 12.5 \text{ J K}^{-1} \text{ mol}^{-1}). These vessels are connected to a manometer tube containing mercury. Initially, the pressure in both vessels is 75 cm75 \text{ cm} of mercury and the temperature is 300 K300 \text{ K}. Subsequently, 5.0 J5.0 \text{ J} of heat is supplied to the gas in vessel AA and 10 J10 \text{ J} to the gas in vessel BB. Assuming no appreciable transfer of heat from AA to BB, calculate the difference in the heights of mercury in the two sides of the manometer. Take the gas constant R=8.3 J K−1 mol−1R = 8.3 \text{ J K}^{-1} \text{ mol}^{-1}.
Two rigid vessels A and B , each having a volume of 200 cm^3 , contain an ideal gas ( C_V = 12.5 J K^ -1 mol^ -1 ).

Options

  1. A8.3 cm8.3 \text{ cm}
  2. B25.0 cm25.0 \text{ cm}
  3. C12.5 cm12.5 \text{ cm}
  4. D6.25 cm6.25 \text{ cm}

Correct answer

C. 12.5 cm12.5 \text{ cm}

Step-by-step solution

For a constant volume process, the heat supplied is Q=nCVΔTQ = n C_V \Delta T.

From the ideal gas equation PV=nRTPV = nRT, the change in pressure at constant volume is ΔP=nRΔTV\Delta P = \dfrac{n R \Delta T}{V}.

Substituting nΔT=QCVn \Delta T = \dfrac{Q}{C_V}, we get ΔP=RQVCV\Delta P = \dfrac{R Q}{V C_V}.

The difference in pressure between vessel B and vessel A is:
ΔPnet=ΔPB−ΔPA=RVCV(QB−QA)\Delta P_{net} = \Delta P_B - \Delta P_A = \dfrac{R}{V C_V} (Q_B - Q_A)

Substituting the given values (R=8.3 J K−1 mol−1R = 8.3 \text{ J K}^{-1} \text{ mol}^{-1}, V=200×10−6 m3V = 200 \times 10^{-6} \text{ m}^3, CV=12.5 J K−1 mol−1C_V = 12.5 \text{ J K}^{-1} \text{ mol}^{-1}, QB−QA=5.0 JQ_B - Q_A = 5.0 \text{ J}):
ΔPnet=8.3×5.02×10−4×12.5=16600 N m−2\Delta P_{net} = \dfrac{8.3 \times 5.0}{2 \times 10^{-4} \times 12.5} = 16600 \text{ N m}^{-2}

To convert this pressure difference into cm of Hg, we use ρHg=13600 kg m−3\rho_{Hg} = 13600 \text{ kg m}^{-3} and g=9.8 m s−2g = 9.8 \text{ m s}^{-2}:
1 cm of Hg=0.01×13600×9.8=1332.8 N m−21 \text{ cm of Hg} = 0.01 \times 13600 \times 9.8 = 1332.8 \text{ N m}^{-2}

The difference in height hh is:
h=166001332.8≈12.45 cmh = \dfrac{16600}{1332.8} \approx 12.45 \text{ cm}

This value is approximately 12.5 cm12.5 \text{ cm}.

Answer: 12.5 cm12.5 \text{ cm}
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