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Question: A gas originally at 1.10 atm and 298 K, underwent a reversible adiabatic expansion to 1.00 atm and 2...

A gas originally at 1.10 atm and 298 K, underwent a reversible adiabatic expansion to 1.00 atm and 287 K. What is the molar heat capacity of the gas at constant pressure? (use log 287 = 2.45, log 298 = 2.47 and log 110 = 2.04139)

Answer

4.1

Explanation

Solution

The relationship between temperature and pressure for a reversible adiabatic process is given by:

T1/T2=(P1/P2)(γ1)/γT_1/T_2 = (P_1/P_2)^{(\gamma-1)/\gamma}

Given:

T1=298T_1 = 298 K, P1=1.10P_1 = 1.10 atm T2=287T_2 = 287 K, P2=1.00P_2 = 1.00 atm

Substitute the values:

298/287=(1.10/1.00)(γ1)/γ298/287 = (1.10/1.00)^{(\gamma-1)/\gamma} 298/287=(1.1)(γ1)/γ298/287 = (1.1)^{(\gamma-1)/\gamma}

Take the logarithm (base 10) of both sides:

log(298/287)=(γ1)/γlog(1.1)\log(298/287) = (\gamma-1)/\gamma \log(1.1) log298log287=(γ1)/γ(log1.1)\log 298 - \log 287 = (\gamma-1)/\gamma (\log 1.1)

We are given the values: log287=2.45\log 287 = 2.45, log298=2.47\log 298 = 2.47, and log110=2.04139\log 110 = 2.04139. Using the given values: log298log287=2.472.45=0.02\log 298 - \log 287 = 2.47 - 2.45 = 0.02

For log1.1\log 1.1: log1.1=log(11/10)=log(110/100)=log110log100=2.041392=0.04139\log 1.1 = \log(11/10) = \log(110/100) = \log 110 - \log 100 = 2.04139 - 2 = 0.04139.

Substitute these values into the logarithmic equation: 0.02=(γ1)/γ×0.041390.02 = (\gamma-1)/\gamma \times 0.04139

Solve for (γ1)/γ(\gamma-1)/\gamma: (γ1)/γ=0.02/0.04139(\gamma-1)/\gamma = 0.02 / 0.04139 (γ1)/γ0.48321(\gamma-1)/\gamma \approx 0.48321

For an ideal gas, the relation between γ\gamma, CpC_p, and the gas constant RR is: γ=Cp/Cv\gamma = C_p/C_v and CpCv=RC_p - C_v = R. From these, we can derive: (γ1)/γ=(Cp/Cv1)/(Cp/Cv)=(CpCv)/Cp=R/Cp(\gamma-1)/\gamma = (C_p/C_v - 1) / (C_p/C_v) = (C_p - C_v)/C_p = R/C_p.

So, we have R/Cp=(γ1)/γR/C_p = (\gamma-1)/\gamma. R/Cp0.48321R/C_p \approx 0.48321

We need to find CpC_p. Cp=R/0.48321C_p = R / 0.48321. The unit of molar heat capacity is typically J/(mol·K) or cal/(mol·K). The gas constant RR has values R=8.314R = 8.314 J/(mol·K) or R1.987R \approx 1.987 cal/(mol·K).

Let's calculate CpC_p using R1.987R \approx 1.987 cal/(mol·K): Cp=1.987/0.483214.1121C_p = 1.987 / 0.48321 \approx 4.1121 cal/(mol·K).

This value is very close to 4.1. The difference is likely due to the rounding of the provided log values. If we assume the expected answer is 4.1, it strongly suggests that the calculation is done using RR in cal/(mol·K) and the provided log values.

Let's check if using R=2R=2 cal/(mol·K) gets us closer: Cp=2/0.483214.139C_p = 2 / 0.48321 \approx 4.139.

The result 4.1121 obtained using R=1.987R=1.987 is closer to 4.1.

Thus, the molar heat capacity of the gas at constant pressure is approximately 4.1 cal/(mol·K).

The final answer is 4.1.