Consider the following two-step process. Heat is allowed to flow out of an ideal gas at constant volume so that its pressure drops from 2.2 atm to 1.4 atm. Then the gas expands at constant pressure, from a volume of 5.9 L to 9.3 L, where the temperature reaches its original value. Calculate (a) the total work done by the gas in the process, (b) the change in internal energy of the gas in the process, and (c) the total heat flow into or out of the gas.
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Problem 58c
Textbook Question
A 100 cm³ box contains helium at a pressure of 2.0 atm and a temperature of 100℃. It is placed in thermal contact with a 200 cm³ box containing argon at a pressure of 4.0 atm and a temperature of 400℃. How much heat energy is transferred, and in which direction?

1
Step 1: Begin by identifying the key variables for each gas. For helium, the initial pressure (P₁) is 2.0 atm, the initial temperature (T₁) is 100℃ (convert to Kelvin: T₁ = 100 + 273 = 373 K), and the volume (V₁) is 100 cm³. For argon, the initial pressure (P₂) is 4.0 atm, the initial temperature (T₂) is 400℃ (convert to Kelvin: T₂ = 400 + 273 = 673 K), and the volume (V₂) is 200 cm³.
Step 2: Use the ideal gas law, \( PV = nRT \), to calculate the number of moles (n) for each gas. For helium: \( n₁ = \frac{P₁ V₁}{RT₁} \), where R is the universal gas constant (8.314 J/(mol·K)). For argon: \( n₂ = \frac{P₂ V₂}{RT₂} \). Substitute the given values to find \( n₁ \) and \( n₂ \).
Step 3: Determine the final equilibrium temperature (Tₓ) after thermal contact. Since heat transfer occurs until thermal equilibrium is reached, use the principle of conservation of energy: \( Q_{helium} + Q_{argon} = 0 \). The heat transferred for each gas is given by \( Q = nC_v \Delta T \), where \( C_v \) is the molar specific heat at constant volume. For monatomic gases like helium and argon, \( C_v = \frac{3}{2}R \). Set up the equation \( n₁C_v(Tₓ - T₁) + n₂C_v(Tₓ - T₂) = 0 \) and solve for \( Tₓ \).
Step 4: Calculate the heat energy transferred for each gas using \( Q = nC_v \Delta T \). For helium: \( Q_{helium} = n₁C_v(Tₓ - T₁) \). For argon: \( Q_{argon} = n₂C_v(Tₓ - T₂) \). Substitute the values of \( n₁ \), \( n₂ \), \( C_v \), and \( Tₓ \) to find the magnitude of heat transferred for each gas.
Step 5: Determine the direction of heat transfer. If \( Q_{helium} > 0 \), heat is absorbed by helium, and if \( Q_{helium} < 0 \), heat is released by helium. Similarly, analyze \( Q_{argon} \). The direction of heat transfer will be from the hotter gas (argon) to the cooler gas (helium) until equilibrium is reached.

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Key Concepts
Here are the essential concepts you must grasp in order to answer the question correctly.
Thermal Energy Transfer
Thermal energy transfer refers to the movement of heat from one body or system to another due to a temperature difference. Heat flows from the hotter object to the cooler one until thermal equilibrium is reached. In this scenario, the heat will transfer from the argon gas at 400℃ to the helium gas at 100℃, as the argon is at a higher temperature.
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Ideal Gas Law
The Ideal Gas Law, expressed as PV = nRT, relates the pressure (P), volume (V), and temperature (T) of an ideal gas to the number of moles (n) and the universal gas constant (R). This law is essential for calculating the properties of gases in the boxes, allowing us to determine how changes in temperature and pressure affect the gases' behavior and energy content.
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Specific Heat Capacity
Specific heat capacity is the amount of heat required to raise the temperature of a unit mass of a substance by one degree Celsius. It is crucial for calculating the heat energy transferred between the helium and argon gases. Knowing the specific heat capacities of both gases allows us to quantify the heat transfer during the thermal interaction between the two boxes.
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