/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 23 An experimenter adds \(970 \math... [FREE SOLUTION] | 91Ó°ÊÓ

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An experimenter adds \(970 \mathrm{~J}\) of heat to \(1.75 \mathrm{~mol}\) of an ideal gas to heat it from \(10.0^{\circ} \mathrm{C}\) to \(25.0^{\circ} \mathrm{C}\) at constant pressure. The gas does \(+223 \mathrm{~J}\) of work during the expansion. (a) Calculate the change in internal energy of the gas. (b) Calculate \(\gamma\) for the gas.

Short Answer

Expert verified
The change in internal energy of the gas is 747 Joules. The specific heat ratio \( \gamma \) of the gas is 4.44.

Step by step solution

01

Calculate the Change in Internal Energy

Start by applying the First Law of Thermodynamics, which is \[ \Delta U = Q - W \] where \( \Delta U \) is the change in internal energy, \( Q \) is the heat added to the system (970 J), and \( W \) is the work done by the system (223 J). Substituting these values yields \( \Delta U = 970 J - 223 J = 747 J \).
02

Compute the Change in Temperature in Kelvin

Temperature changes are measured in Kelvin in thermodynamics. Consequently, both temperatures need to be converted into Kelvin and the difference obtained: \( \Delta T = T_{\text{final}} - T_{\text{initial}} = 25^\circ C + 273.15 - (10^\circ C + 273.15 K) = 15K \).
03

Calculate the Molar Specific Heat at Constant Pressure \( C_p \)

To find \( C_p \), we use the formula \( Q = n \cdot C_p \cdot \Delta T \) where \( n \) represents the number of moles (1.75 mol). Rearranging for \( C_p = Q / (n \cdot \Delta T) \) and substituting the available figures: \( C_p = \frac{970 J}{1.75 mol \cdot 15 K} = \frac{970 J}{26.25 mol \cdot K} = 36.95 J/(mol \cdot K) \).
04

Calculate \( \gamma \)

The value of \( \gamma \) can be calculated using the equation \( C_p = \gamma R \) where \( R \) is the universal gas constant (8.3145 J/(mol*K)). We rearrange to solve for \( \gamma = \frac{C_p}{R} = \frac{36.95 J/(mol \cdot K) }{ 8.3145 J/(mol*K)} = 4.44 \).

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Key Concepts

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

Internal Energy Change
Internal energy is a key element in understanding thermodynamic systems, and the First Law of Thermodynamics helps us determine how this energy changes. The law is succinctly expressed as the equation \[ \Delta U = Q - W \], where \( \Delta U \) represents the change in internal energy, \( Q \) denotes the heat added to the system, and \( W \) indicates the work done by the system.

In the context of our exercise, when heat is added to a gas at constant pressure, and the gas expands doing work, the internal energy change can be calculated by subtracting the work done from the heat added. Following the exercise, after adding 970 J of heat and performing 223 J of work, the internal energy increases by 747 J, which accounts for the net energy staying within the system after some of it has been used to perform expansion work.

Grasping this concept is pivotal because the internal energy denotes the total energy within a thermodynamic system, a critical factor in predicting the system's behavior under various conditions.
Molar Specific Heat at Constant Pressure
The molar specific heat at constant pressure, denoted as \( C_p \), is a measurement of the amount of heat energy required to increase the temperature of one mole of a substance by one Kelvin at constant pressure. In a practical sense, this is a property that tells us how 'heat resistant' a substance is. The more heat is needed to change the temperature, the higher the \( C_p \).

As demonstrated in the exercise, the formula used to determine \( C_p \) is \[ Q = n \cdot C_p \cdot \Delta T \], where \( n \) is the number of moles and \( \Delta T \) is the change in temperature in Kelvin. By rearranging the formula, we get \( C_p = Q / (n \cdot \Delta T) \). When this formula is applied to the exercise's scenario, we find that the gas's \( C_p \) equals 36.95 J/(mol \cdot K), providing us with the requisite information to further investigate the properties of the gas.
Heat Capacity Ratio
The heat capacity ratio, often symbolized by \( \gamma \), is the ratio of the molar specific heats of a gas at constant pressure \( C_p \) to that at constant volume \( C_v \). This ratio \( \gamma = C_p / C_v \) is particularly important in thermodynamics as it describes the relationship between pressure and volume under adiabatic processes for an ideal gas.

In the problem from the textbook, we take an alternate approach by considering the relationship \( C_p = \gamma R \) where \( R \) is the universal gas constant. By calculating \( \gamma \) as 4.44 from the given problem, we can infer certain behaviors of the gas. A higher \( \gamma \) often indicates a larger difference between \( C_p \) and \( C_v \) and characterizes how gases expand or compress under certain conditions. Understanding this ratio is paramount because it can help predict how much work a gas can do when expanding adiabatically, which is crucial in designing engines and understanding atmospheric processes.

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Most popular questions from this chapter

\( \mathrm{A}\) gas in a cylinder is held at a constant pressure of \(1.80 \times 10^{5} \mathrm{~Pa}\) and is cooled and compressed from \(1.70 \mathrm{~m}^{3}\) to \(1.20 \mathrm{~m}^{3}\). The internal energy of the gas decreases by \(1.40 \times 10^{5} \mathrm{~J}\). (a) Find the work done by the gas. (b) Find the absolute value of the heat flow, \(|Q|\), into or out of the gas, and state the direction of the heat flow. (c) Does it matter whether the gas is ideal? Why or why not?

A cylinder with a piston contains \(0.150 \mathrm{~mol}\) of nitrogen at \(1.80 \times 10^{5} \mathrm{~Pa}\) and \(300 \mathrm{~K}\). The nitrogen may be treated as an ideal gas. The gas is first compressed isobarically to half its original volume. It then expands adiabatically back to its original volume, and finally it is heated isochorically to its original pressure. (a) Show the series of processes in a \(p V\) -diagram. (b) Compute the temperatures at the beginning and end of the adiabatic expansion. (c) Compute the minimum pressure.

On a warm summer day, a large mass of air (atmospheric pressure \(1.01 \times 10^{5} \mathrm{~Pa}\) ) is heated by the ground to \(26.0^{\circ} \mathrm{C}\) and then begins to rise through the cooler surrounding air. (This can be treated approximately as an adiabatic process; why?) Calculate the temperature of the air mass when it has risen to a level at which atmospheric pressure is only \(0.850 \times 10^{5} \mathrm{~Pa}\). Assume that air is an ideal gas, with \(\gamma=1.40\). (This rate of cooling for dry, rising air, corresponding to roughly \(1 \mathrm{C}^{\circ}\) per \(100 \mathrm{~m}\) of altitude, is called the \(d r y\) adiabatic lapse rate.

A gas undergoes two processes. In the first, the volume remains constant at \(0.200 \mathrm{~m}^{3}\) and the pressure increases from \(2.00 \times 10^{5} \mathrm{~Pa}\) to \(5.00 \times 10^{5} \mathrm{~Pa}\). The second process is a compression to a volume of \(0.120 \mathrm{~m}^{3}\) at a constant pressure of \(5.00 \times 10^{5} \mathrm{~Pa}\). (a) In a \(p V\) -diagram, show both processes. (b) Find the total work done by the gas during both processes.

\( \mathrm{A}\) gas in a cylinder expands from a volume of \(0.110 \mathrm{~m}^{3}\) to \(0.320 \mathrm{~m}^{3} .\) Heat flows into the gas just rapidly enough to keep the pres- sure constant at \(1.65 \times 10^{5} \mathrm{~Pa}\) during the expansion. The total heat added is \(1.15 \times 10^{5} \mathrm{~J}\). (a) Find the work done by the gas. (b) Find the change in internal energy of the gas. (c) Does it matter whether the gas is ideal? Why or why not?

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