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An air pump has a cylinder \(0.250 \mathrm{~m}\) long with a movable piston. The pump is used to compress air from the atmosphere (at absolute pressure \(1.01 \times 10^{5} \mathrm{~Pa}\) ) into a very large tank at \(3.80 \times 10^{5} \mathrm{~Pa}\) gauge pressure. (For air, \(\left.C_{V}=20.8 \mathrm{~J} / \mathrm{mol} \cdot \mathrm{K} .\right)\) (a) The piston begins the compression stroke at the open end of the cylinder. How far down the length of the cylinder has the piston moved when air first begins to flow from the cylinder into the tank? Assume that the compression is adiabatic. (b) If the air is taken into the pump at \(27.0^{\circ} \mathrm{C},\) what is the temperature of the compressed air? (c) How much work does the pump do in putting \(20.0 \mathrm{~mol}\) of air into the tank?

Short Answer

Expert verified
The displacement of the piston is calculated as \(0.0892 m\). The temperature of the compressed air is calculated as \(446.59 K\) (or \(173.44^{\circ}C\)). The work done by the pump is calculated as \(83411.60 J\).

Step by step solution

01

Finding displacement of the piston

Initially, the pressure \(P_{1}\) was atmospheric pressure \(1.01 \times 10^{5} Pa\) and the volume \(V_{1}\) is assumed to be the full cylinder volume. Air enters the tank when pressure in cylinder \(P_{2}\) reaches the tank pressure, which is atmospheric pressure plus the gauge pressure, \(1.01 \times 10^{5} Pa + 3.80 \times 10^{5} Pa = 4.81 \times 10^{5} Pa\). If we define \(V_{2}\) as the volume the air takes up when it reaches the tank pressure, we can relate the initial state of the air \((P_{1}, V_{1})\) to its final state \((P_{2}, V_{2})\) using the adiabatic relation \(P_{1}V_{1}^{γ} = P_{2}V_{2}^{γ}\), where \(γ = C_{P}/C_{V}\) for diatomic molecules like air, and is approx 1.4. We solve for \(V_{2}\) and remember that the volume difference \((V_{1} - V_{2})\) represents the cylinder volume displaced by the piston until the air enters the tank.
02

Finding the temperature of the compressed air

We again use the adiabatic relation, but now to find the temperature of the compressed air (\(T_{2}\)), using the relationship between volume and temperature during an adiabatic process which is \(T_{1}V_{1}^{γ-1} = T_{2}V_{2}^{γ-1}\). The initial temperature \(T_{1}\) is 27.0 degrees Celsius, but it must be converted to Kelvin by adding 273.15. We use the volume \(V_{2}\) from Step 1 and solve for \(T_{2}\).
03

Finding the work done by the pump

The work done by the pump is given by \(W = nC_{V}(T_{2} - T_{1})\) where n is the number of moles \(20.0 mol\) and \(C_{V}\) is the molar specific heat \(20.8 J/(mol.K)\). We use the initial temperature \(T_{1}\) and the final temperature \(T_{2}\) from the previous step and solve for \(W\).

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Key Concepts

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

Absolute Pressure
Understanding absolute pressure is vital when studying gas behaviors under different conditions. This term refers to the total pressure exerted on a system, including atmospheric pressure and any additional pressure caused by forces applied to the system. For instance, when an air pump compresses air into a tank, the absolute pressure is a sum of the atmospheric pressure and the pressure exerted by the pump.

In thermodynamics, it is essential to use absolute pressure to accurately describe the state of a gas. When we talk about an air pump compressing air from an atmospheric absolute pressure of \(1.01 \times 10^{5} \mathrm{~Pa}\) to a tank with a gauge pressure, we consider the atmospheric pressure in addition to the air pump's contribution to determine the final absolute pressure in the tank. This understanding is particularly crucial when applying the adiabatic process equations to determine the amount of work done by the pump or the final temperature of the compressed air.

For instance, in the exercise regarding adiabatic compression, we combined atmospheric pressure with gauge pressure to obtain the total absolute pressure in the tank, which plays a critical role in subsequent calculations, such as the displacement of the piston.
Gauge Pressure
Gauge pressure is another fundamental concept in understanding pressure systems—it is the pressure that is measured relative to the atmospheric pressure. Unlike absolute pressure, which measures the total pressure including the atmosphere, gauge pressure only shows the difference between the system's pressure and the atmospheric pressure.

For example, when a pressure gauge on a tank reads \(3.80 \times 10^{5} \mathrm{~Pa}\), this is the gauge pressure, meaning it is the pressure above and beyond atmospheric pressure. To find the absolute pressure in the air tank in our exercise, we need to add atmospheric pressure to the gauge pressure. The understanding of gauge pressure helped us figure out when the air would begin to flow from the cylinder into the tank, based on the information given in the original question.
Molar Specific Heat
The molar specific heat of a substance is a measure of how much energy in the form of heat is needed to raise the temperature of one mole of the substance by one degree Celsius (or one Kelvin), at constant volume or pressure. In our case, \(C_{V}\) represents the molar specific heat at constant volume, and it’s an intrinsic property of the substance (air in this exercise) involved.

In the context of adiabatic compression, \(C_{V}\) is used to calculate the work done by the pump, as well as the change in temperature of the air. Specifically, the formula \(W = nC_{V}(T_{2} - T_{1})\) incorporates molar specific heat at constant volume to calculate the work done when compressing \(20.0 \mathrm{~mol}\) of air. By knowing \(C_{V}\), and the temperatures before and after compression, we can derive the total work done by the pump during the adiabatic compression process, as shown in the final step of the exercise solution.
Thermodynamics
At its core, thermodynamics is the study of energy, heat, and work, and how they relate to each other within different systems. This field of physics plays an indispensable role in tasks such as calculating the work done during adiabatic compression, or determining the final temperature of a gas after compression.

Adiabatic processes, a key concept in thermodynamics, are transformations that occur without any heat being transferred to or from the surroundings. The steps used in solving the exercise demonstrate thermodynamic principles in action. We applied the adiabatic relation \(P_{1}V_{1}^{\gamma} = P_{2}V_{2}^{\gamma}\) to link the initial and final states of the air during compression. Furthermore, understanding the relationship between pressure, volume, and temperature is essential to solving real-world problems involving gas compression and expansion.

When we solved for the displacement of the piston and the temperature of the compressed air, we employed the concepts of initial and final states. These are crucial in thermodynamics to predict the outcome of a process — such as how the temperature will increase during adiabatic compression. All the steps in our exercise reflected the laws of thermodynamics, which govern the transitions and flows of energy within systems.

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Most popular questions from this chapter

A thermodynamic system undergoes processes in which \(|Q|=100 \mathrm{~J}\) and \(|W|=300 \mathrm{~J}\). Find \(Q\) and \(W,\) including whether the quantity is positive or negative, if the change in internal energy is (a) \(+400 \mathrm{~J},(\mathrm{~b})+200 \mathrm{~J},(\mathrm{c})-200 \mathrm{~J},\) and \((\mathrm{d})-400 \mathrm{~J} .\)

Helium gas undergoes an adiabatic process in which the Kelvin temperature doubles. By what factor does the pressure change?

Comparing Thermodynamic Processes. In a cylinder, \(1.20 \mathrm{~mol}\) of an ideal monatomic gas, initially at \(3.60 \times 10^{5} \mathrm{~Pa}\) and \(300 \mathrm{~K},\) expands until its volume triples. Compute the work done by the gas if the expansion is (a) isothermal; (b) adiabatic; (c) isobaric. (d) Show each process in a \(p V\) -diagram. In which case is the absolute value of the work done by the gas greatest? Least? (e) In which case is the absolute value of the heat transfer greatest? Least? (f) In which case is the absolute value of the change in internal energy of the gas greatest? Least?

A steel cargo drum has a height of \(880 \mathrm{~mm}\) and a diameter of \(610 \mathrm{~mm}\). With its top removed it has a mass of \(17.3 \mathrm{~kg}\). The drum is turned upside down at the surface of the North Atlantic and is pulled downward into the ocean by a robotic submarine. On this day the surface temperature is \(23.0^{\circ} \mathrm{C}\) and the surface air pressure is \(p_{0}=101 \mathrm{kPa}\). The water temperature decreases linearly with depth to \(3.0^{\circ} \mathrm{C}\) at \(1000 \mathrm{~m}\) below the surface. As the drum moves downward in the ocean, the air inside the drum is compressed, reducing the upward buoyant force. (a) At what depth \(y_{\text {neutral }}\) is the barrel neutrally buoyant? (Hint: The pressure in the drum is equal to the sea pressure, which at depth \(y\) is \(p_{0}+\rho g y\) where \(\rho=1025 \mathrm{~kg} / \mathrm{m}^{3}\) is the density of seawater. The temperature at depth can be determined using the information above. Together with the ideal- gas law, you can derive a formula for the volume of air at depth \(y,\) and therefore a formula for the upward buoyant force as a function of depth.) (b) What is the volume of the air in the drum at depth \(y_{\text {neutral }} ?\)

A cylinder with a piston contains \(0.250 \mathrm{~mol}\) of oxygen at \(2.40 \times 10^{5} \mathrm{~Pa}\) and \(355 \mathrm{~K}\). The oxygen may be treated as an ideal gas. The gas first expands isobarically to twice its original volume. It is then compressed isothermally back to its original volume, and finally it is cooled isochorically to its original pressure. (a) Show the series of processes on a \(p V\) -diagram. Compute (b) the temperature during the isothermal compression; (c) the maximum pressure; (d) the total work done by the piston on the gas during the series of processes.

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