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A \(1 \mathrm{~m}^{3}\) tank initially contains air at \(300 \mathrm{kPa}, 300 \mathrm{~K}\). Air slowly escapes from the tank until the pressure drops to 100 \(\mathrm{kPa}\). The air that remains in the tank undergoes a process described by \(p v^{1.2}=\) constant. For a control volume enclosing the tank, determine the heat transfer, in kJ. Assume ideal gas behavior with constant specific heats.

Short Answer

Expert verified
The heat transfer is -123.7 kJ.

Step by step solution

01

Identify initial and final states

Initial State: \[P_1 = 300 \text{ kPa}, \, V_1 = 1 \text{ m}^3, \, T_1 = 300 \text{ K}\] Final State: \[P_2 = 100 \text{ kPa} \text{ and the process follows } p v^{1.2} = \text{constant}\]
02

Relate volumes using polytropic process

For a polytropic process, \(P_1 V_1^{1.2} = P_2 V_2^{1.2}\). Thus, we can solve for \(V_2\): \[V_2 = V_1 \left(\frac{P_1}{P_2}\right)^{\frac{1}{1.2}}\] Substitute the given values: \[V_2 = 1 \text{ m}^3 \left(\frac{300 \text{ kPa}}{100 \text{ kPa}}\right)^{\frac{1}{1.2}} = 2.143\text{ m}^3\]
03

Determine the final temperature

Using the ideal gas law, the specific volume \(v\) at state 1 is: \[v_1 = \frac{V_1}{\text{mass}} = \frac{RT_1}{P_1}\] And for state 2: \[v_2 = \frac{V_2}{\text{mass}} = \frac{RT_2}{P_2}\] Relating the temperatures using the polytropic process equation, and assuming \(R\) is constant, we get: \[T_2 = T_1 \left(\frac{V_2}{V_1}\right)^{1-1.2} = 300 \text{ K} \left(2.143\right)^{-0.2} = 251 \text{ K}\]
04

Calculate internal energy change

The internal energy change \(\Delta U\) can be calculated using: \[\Delta U = m c_v (T_2 - T_1)\] Calculating mass \(m\) using \(P_1 V_1 = m R T_1\): \[m = \frac{P_1 V_1}{R T_1} = \frac{300 \text{ kPa} \times 1 \text{ m}^3}{0.287 \text{ kJ/kg⋅K} \times 300 \text{ K}} = 3.484 \text{ kg}\] Specific heat at constant volume \(c_v\) for air is approximately \(0.718 \text{ kJ/kg⋅K}\). Hence: \[\Delta U = 3.484 \text{ kg} \times 0.718 \text{ kJ/kg⋅K} \times (251 \text{ K} - 300 \text{ K}) = -123.7 \text{ kJ}\]
05

Apply the first law of thermodynamics

The first law of thermodynamics for a control volume is given by: \[\Delta U = Q - W\] Since there is no work done (volume change at constant pressure), \(W = 0\). Therefore, the heat transfer \(Q\) is: \[Q = \Delta U = -123.7 \text{ kJ}\]

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Ideal Gas Law
The Ideal Gas Law is a fundamental principle in thermodynamics, describing the state of an ideal gas using the equation of state:\[ PV = nRT \]where \( P \) stands for pressure, \( V \) for volume, \( n \) for the number of moles, \( R \) for the universal gas constant, and \( T \) for temperature in Kelvin. This law helps us understand relationships between these properties in gaseous systems.In our exercise, we applied the ideal gas law at different states (initial and final) to determine quantities like mass and temperature change.
To apply the ideal gas law correctly, make sure you:
  • Use consistent units for pressure (Pa, kPa), volume (m³), and temperature (K).
  • Use the specific gas constant for air, which approximately is \( 0.287 \text{ kJ/kg·K} \).

The ideal gas law simplification assumes no intermolecular forces, thus only holds exactly true under specific conditions:
  • High temperatures
  • Low pressures
But it provides a good approximation for many practical situations.
Internal Energy Change
Internal energy change (\(\Delta U\)) is a measure of the energy gained or lost by a system due to changes in temperature. For an ideal gas, the formula to calculate this change is: \[ \Delta U = m c_v \Delta T \]where \(m\) represents the mass of the gas, \(c_v\) the specific heat at constant volume, and \(\Delta T\) the temperature change.Let's break down the steps to calculate internal energy change more fully:
  • Firstly, determine the mass of the gas using: \( m = \frac{P_1 V_1}{R T_1} \).
  • This mass helps in computing the change in internal energy when temperature changes from \( T_1 \) to \( T_2 \).
  • For air, a common value for \( c_v \) is around 0.718 kJ/kgK.

In our exercise:
  • \(m\) = 3.484 kg was calculated using the initial state properties.
  • Then we used this to compute \( \Delta U = 3.484 \times 0.718 \times (251 - 300) = -123.7 \text{kJ} \).
A negative \( \Delta U \) indicates the system lost energy. Thus, internal energy changes directly correlate with temperature changes, considering specific heat and gas mass.
First Law of Thermodynamics
The First Law of Thermodynamics establishes the principle of energy conservation in thermodynamic systems. It states: \[ \Delta U = Q - W \]where \( \Delta U \) is the change in internal energy, \( Q \) is the heat transfer into the system, and \( W \) is the work done by the system.In our particular exercise, we found:
  • \(W\) was zero because there was no work done (isobaric volume change).
  • Thus, the change in internal energy equaled the heat transfer (\( Q = \Delta U = -123.7 \text{kJ} \)).
This law is crucial for solving many engineering and physics problems as it concretely links energy changes in a system to heat transfer and work done. To apply this law effectively:
  • Always define the system boundary and assess if work or heat transfer occurs across it.
  • Use appropriate signs: positive for heat added to the system and negative for heat lost.

By adhering to the first law, we ensure that energy is neither created nor destroyed but transformed from one form to another. This understanding allows us to solve for unknown quantities in diverse thermodynamic processes.

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Most popular questions from this chapter

Methods for measuring mass flow rates of gases and liquids flowing in pipes and ducts include: rotameters, turbine flowmeters, orifice-type flowmeters, thermal flowmeters, and Coriolis-type flowmeters. Determine the principles of operation of each of these flow-measuring devices. Consider the suitability of each for measuring liquid or gas flows. Can any be used for two-phase liquid- vapor mixtures? Which measure volumetric flow rate and require separate measurements of pressure and temperature to determine the state of the substance? Summarize your findings in a brief report.

Air enters a compressor operating at steady state with a pressure of 1 bar, a temperature of \(20^{\circ} \mathrm{C}\), and a volumetric flow rate of \(0.25 \mathrm{~m}^{3} / \mathrm{s}\). The air velocity in the exit pipe is \(210 \mathrm{~m} / \mathrm{s}\) and the exit pressure is \(1 \mathrm{MPa}\). If each unit mass of air passing from inlet to exit undergoes a process described by \(p v^{1.34}=\) constant, determine the exit temperature, in \({ }^{\circ} \mathrm{C}\).

Does \(\dot{Q}_{\mathrm{cv}}\) accounting for energy transfer by heat include heat transfer across inlets and exits? Under what circumstances might heat transfer across an inlet or exit be significant?

Nitrogen gas enters a turbine operating at steady state with a velocity of \(60 \mathrm{~m} / \mathrm{s}\), a pressure of \(0.345 \mathrm{Mpa}\), and a temperature of \(700 \mathrm{~K}\). At the exit, the velocity is \(0.6 \mathrm{~m} / \mathrm{s}\), the pressure is \(0.14 \mathrm{Mpa}\), and the temperature is \(390 \mathrm{~K}\). Heat transfer from the surface of the turbine to the surroundings occurs at a rate of \(36 \mathrm{~kJ}\) per \(\mathrm{kg}\) of nitrogen flowing. Neglecting potential energy effects and using the ideal gas model, determine the power developed by the turbine, in \(\mathrm{kW}\).

A tank of volume \(1 \mathrm{~m}^{3}\) initially contains steam at \(6 \mathrm{MPa}\) and \(320^{\circ} \mathrm{C}\). Steam is withdrawn slowly from the tank until the pressure drops to \(p\). Heat transfer to the tank contents maintains the temperature constant at \(320^{\circ} \mathrm{C}\). Neglecting all kinetic and potential energy effects (a) determine the heat transfer, in \(\mathrm{kJ}\), if \(p=1.5 \mathrm{MPa}\). (b) plot the heat transfer, in \(\mathrm{kJ}\), versus \(p\) ranging from \(0.5\) to \(6 \mathrm{MPa}\).

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