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Give step-by-step solution with explanation and final answer: Consider 5 kg of oxygen, initially at 2 0 0 K and 8 0 kPa , undergoing an isobaric process doubling its volume, then an isochoric process doubling its pressure, an isothermal expansion reducing its pressure to the initial value, and finally, an adiabatic compression returning to the initial volume. Calculate the enthalpy changes for each of the stages and the total enthalpy change of the system. To do this, you must draw the PV diagram in which the various quasi - static processes undergone by the thermodynamic system must be shown.

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Give step-by-step solution with explanation and final answer: Consider 5 kg of oxygen, initially at 2 0 0 K and 8 0 kPa , undergoing an isobaric process doubling its volume, then an isochoric process doubling its pressure, an isothermal expansion reducing its pressure to the initial value, and finally, an adiabatic compression returning to the initial volume. Calculate the enthalpy changes for each of the stages and the total enthalpy change of the system. To do this, you must draw the PV diagram in which the various quasi - static processes undergone by the thermodynamic system must be shown.

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Asked by: Test User 100044
Created at: 2025-04-26 01:06:55

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Let’s solve the problem step by step: --- ## **Step 1: Initial Data and Constants** - **Mass of \( O_2 \), \( m \):** 5 kg - **Initial Temperature, \( T_1 \):** 200 K - **Initial Pressure, \( P_1 \):** 80 kPa = 80,000 Pa - **Gas Constant for Oxygen, \( R \):** 0.2598 kJ/kg·K = 259.8 J/kg·K - **Specific heat at constant pressure, \( C_p \):** For diatomic gases (like \( O_2 \)), \( C_p = \frac{7}{2} R \) \( C_p = 7/2 \times 259.8 = 909.3 \) J/kg·K --- ## **Step 2: Initial State** Use the ideal gas law: \[ P_1 V_1 = m R T_1 \] \[ V_1 = \frac{m R T_1}{P_1} = \frac{5 \times 259.8 \times 200}{80,000} = \frac{259,800}{80,000} = 3.2475~m^3 \] --- ## **Step 3: Process 1 (1→2): Isobaric Expansion (Volume Doubles)** - \( P_1 = P_2 \) - \( V_2 = 2 V_1 \) Use ideal gas law for state 2: \[ P_2 V_2 = m R T_2 \implies T_2 = \frac{P_2 V_2}{m R} = \frac{P_1 \times 2 V_1}{m R} \] But \( P_1 V_1 = m R T_1 \implies V_1 = \frac{m R T_1}{P_1} \), plug this in: \[ T_2 = \frac{P_1 \times 2 \times \frac{m R T_1}{P_1}}{m R} = 2 T_1 = 2 \times 200 = 400~K \] **Enthalpy change for isobaric process:** \[ \Delta H_{1\to2} = m C_p (T_2 - T_1) = 5 \times 909.3 \times (400-200) = 5 \times 909.3 \times 200 = 909,300~J = \boxed{909.3~kJ} \] --- ## **Step 4: Process 2→3: Isochoric (Volume Constant), Pressure Doubles** - \( V_3 = V_2 = 2 V_1 \) - \( P_3 = 2 P_2 = 2 P_1 = 160~kPa \) Use ideal gas law for state 3: \[ P_3 V_3 = m R T_3 \implies T_3 = \frac{P_3 V_3}{m R} \] But \( P_3 = 2 P_1 \), \( V_3 = 2 V_1 \): \[ T_3 = \frac{2 P_1 \times 2 V_1}{m R} = 4 \frac{P_1 V_1}{mR} = 4 T_1 = 800~K \] **Enthalpy change:** \[ \Delta H_{2\to3} = m C_p (T_3 - T_2) = 5 \times 909.3 \times (800-400) = 5 \times 909.3 \times 400 = 1,818,600~J = \boxed{1,818.6~kJ} \] --- ## **Step 5: Process 3→4: Isothermal Expansion (Temperature Constant at \( T_3 \)), Pressure drops to initial value** - \( T_4 = T_3 = 800~K \) - \( P_4 = P_1 = 80~kPa \) Use ideal gas law to find \( V_4 \): \[ P_4 V_4 = m R T_4 \implies V_4 = \frac{m R T_4}{P_4} \] Plug in values: \[ V_4 = \frac{5 \times 259.8 \times 800}{80,000} = \frac{1,039,200}{80,000} = 12.99~m^3 \] **Enthalpy change for isothermal process:** \[ \Delta H_{3\to4} = m C_p (T_4 - T_3) = 0 \] --- ## **Step 6: Process 4→1: Adiabatic Compression (Returns to Initial Volume, so \( V_1 \)), Find Final Temperature** - \( V_4 \to V_1 \) - \( T_4 = 800~K \) - \( V_1 = 3.2475~m^3 \) - \( V_4 = 12.99~m^3 \) For adiabatic process for an ideal gas: \[ T V^{\gamma-1} = \text{constant} \] where \( \gamma = \frac{C_p}{C_v} = \frac{7}{5} = 1.4 \) for diatomic gases. So, \[ T_4 V_4^{\gamma-1} = T_1 V_1^{\gamma-1} \implies T_1 = T_4 \left( \frac{V_4}{V_1} \right)^{\gamma-1} \] But since \( V_4 > V_1 \), and returning to \( V_1 \): \[ T_1 = T_4 \left( \frac{V_4}{V_1} \right)^{1-\gamma} \] But since we started at \( T_1 = 200~K \), let's check consistency: \[ T_1 = 800 \times \left( \frac{3.2475}{12.99} \right)^{0.4} \] Calculate \( \frac{3.2475}{12.99} = 0.25 \) Then \( 0.25^{0.4} \): \[ \ln(0.25) = -1.3863 \implies -1.3863 \times 0.4 = -0.5545 \implies e^{-0.5545} = 0.574 \] So, \[ T_1 = 800 \times 0.574 = 459~K \] But this does **not** return us to the initial temperature. However, we're told the process returns to the initial volume (not necessarily temperature), so the enthalpy change is: \[ \Delta H_{4\to1} = m C_p (T_1 - T_4) = 5 \times 909.3 \times (200 - 800) = 5 \times 909.3 \times (-600) = -2,727,900~J = \boxed{-2,727.9~kJ} \] But our calculation above for \( T_1 \) says it returns to 459 K, not 200 K. This suggests one of two things: - The process does not return to the initial temperature (only the initial volume), - Or, something is inconsistent in the problem statement. Let's proceed with the calculation as per the correct adiabatic relation: \[ T_1 = T_4 \left( \frac{V_4}{V_1} \right)^{1-\gamma} = 800 \times (4)^{-0.4} \] \( 4^{-0.4} = e^{-0.4 \ln 4} = e^{-0.4 \times 1.3863} = e^{-0.5545} = 0.574 \) So, \[ T_1 = 800 \times 0.574 = 459~K \] So, the final temperature is 459 K. Thus, \[ \Delta H_{4\to1} = m C_p (T_1 - T_4) = 5 \times 909.3 \times (459 - 800) = 5 \times 909.3 \times (-341) = -1,551,196~J = \boxed{-1,551.2~kJ} \] --- ## **Step 7: Total Enthalpy Change** Sum the enthalpy changes for each process: 1. \( 1 \to 2 \): \( +909.3~kJ \) 2. \( 2 \to 3 \): \( +1,818.6~kJ \) 3. \( 3 \to 4 \): \( 0~kJ \) 4. \( 4 \to 1 \): \( -1,551.2~kJ \) \[ \Delta H

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