/*! 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 9 The temperature of \(5.00 \mathr... [FREE SOLUTION] | 91Ó°ÊÓ

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The temperature of \(5.00 \mathrm{~kg}\) of \(\mathrm{N}_{2}\) gas is raised from \(10.0{ }^{\circ} \mathrm{C}\) to \(130.0{ }^{\circ} \mathrm{C}\). If this is done at constant volume, find the increase in internal energy \(\Delta U .\) Alternatively, if the same temperature change now occurs at constant pressure determine both \(\Delta V\) and the external work \(\Delta W\) done by the gas. For \(\mathrm{N}_{2}\) gas, \(c_{v}=0.177 \mathrm{cal} / \mathrm{g} \cdot{ }^{\circ} \mathrm{C}\) and \(c_{p}=0.248 \mathrm{cal} / \mathrm{g} \cdot{ }^{\circ} \mathrm{C}\). If the gas is heated at constant volume, then no work is done during the process. In that case \(\Delta W=0\), and the first law tells us that \((\Delta Q)_{v}=\Delta U .\) Because \((\Delta Q)_{v}=c_{v} m \Delta T\), $$\Delta U=(\Delta Q)_{v}=\left(0.177 \mathrm{cal} / \mathrm{g} \cdot{ }^{\circ} \mathrm{C}\right)(5000 \mathrm{~g})\left(120^{\circ} \mathrm{C}\right)=106 \mathrm{kcal}=443 \mathrm{~kJ}$$ The temperature change is a manifestation of the internal energy change. When the gas is heated \(120^{\circ} \mathrm{C}\) at constant pressure, the same change in internal energy occurs. In addition, however, work is done. The first law then becomes $$(\Delta Q)_{p}=\Delta U+\Delta W=443 \mathrm{~kJ}+\Delta W$$ But $$\begin{aligned} (\Delta Q)_{p} &=c_{p} m \Delta T=\left(0.248 \mathrm{cal} / \mathrm{g} \cdot{ }^{\circ} \mathrm{C}\right)(5000 \mathrm{~g})\left(120{ }^{\circ} \mathrm{C}\right) \\ &=149 \mathrm{kcal}=623 \mathrm{~kJ} \end{aligned}$$ $$ \text { Hence } \quad \Delta W=(\Delta Q)_{p}-\Delta U=623 \mathrm{~kJ}-443 \mathrm{~kJ}=180 \mathrm{~kJ} $$

Short Answer

Expert verified
At constant volume: \(\Delta U = 443 \text{ kJ}\). At constant pressure: \(\Delta V\) not calculated and \(\Delta W = 180 \text{ kJ}\).

Step by step solution

01

Calculate Change in Internal Energy at Constant Volume

When the nitrogen gas is heated at constant volume, no work is done (\(\Delta W = 0\)), and the change in internal energy is equivalent to the heat added \((\Delta Q)_v\). The formula is \(\Delta U = c_v \cdot m \cdot \Delta T\)., where \(c_v = 0.177 \text{ cal/g°C}, m = 5000 \text{ g}, \text{ and } \Delta T = 130.0°C - 10.0°C = 120.0°C\). Thus:\[\Delta U = \left(0.177 \text{ cal/g°C}\right) \times (5000 \text{ g}) \times (120.0°C) = 106 \text{ kcal}\]\Converting to joules, since \(1 \text{ kcal} = 4.184 \text{ kJ}\), this becomes:\[\Delta U = 106 \text{ kcal} \times 4.184 \text{ kJ/kcal} = 443 \text{ kJ}\]The change in internal energy at constant volume is \(443 \text{ kJ}\).
02

Calculate Total Heat Added at Constant Pressure

When the nitrogen gas is heated at constant pressure, the heat added \((\Delta Q)_p\), can be calculated as:\((\Delta Q)_p = c_p \cdot m \cdot \Delta T\), where \(c_p = 0.248 \text{ cal/g°C}, m = 5000 \text{ g}, \text{ and } \Delta T = 120.0°C\). Thus:\[(\Delta Q)_p = (0.248 \text{ cal/g°C}) \times (5000 \text{ g}) \times (120.0°C) = 149 \text{ kcal}\]Converting to joules:\[(\Delta Q)_p = 149 \text{ kcal} \times 4.184 \text{ kJ/kcal} = 623 \text{ kJ}\]The heat added at constant pressure is \(623 \text{ kJ}\).
03

Determine Work Done at Constant Pressure

According to the first law of thermodynamics, at constant pressure, the heat added \((\Delta Q)_p\) is equal to the change in internal energy plus the work done \((\Delta W)\) by the system: \((\Delta Q)_p = \Delta U + \Delta W\).We already know:\(\Delta Q_p = 623 \text{ kJ}\) and\(\Delta U = 443 \text{ kJ}\).Thus, rearranging the formula gives:\[\Delta W = (\Delta Q)_p - \Delta U = 623 \text{ kJ} - 443 \text{ kJ} = 180 \text{ kJ}\]The work done by the gas at constant pressure is \(180 \text{ kJ}\).

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Key Concepts

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

First Law of Thermodynamics
The First Law of Thermodynamics is a fundamental principle that connects internal energy, heat, and work. It states that the energy of an isolated system remains constant. This means that energy can neither be created nor destroyed, only transformed or transferred. The formula often used is\[ \Delta U = \Delta Q - \Delta W \]where \( \Delta U \) is the change in internal energy, \( \Delta Q \) is the heat added to the system, and \( \Delta W \) is the work done by the system.

This law is essentially about energy conservation. For instance, in our exercise, when the gas is heated at constant volume, no work is done, so all heat energy goes into changing the internal energy. However, at constant pressure, part of the energy goes into doing work by expanding the gas.
Internal Energy
The internal energy of a system refers to the total energy contained within it, arising from the kinetic and potential energies of its molecules. This concept forms the foundation for understanding changes in temperature and phase.

When the gas was heated, the rise in temperature signified an increase in kinetic energy, thus increasing the internal energy. This energy change is calculated using the formula:\[ \Delta U = c_v \cdot m \cdot \Delta T \]where \( c_v \) is the specific heat capacity at constant volume, \( m \) is the mass, and \( \Delta T \) is the temperature change.

In our example, this helped us find that the internal energy change of the nitrogen gas was 443 kJ.
Heat Capacity
Heat capacity is an important property that describes how much heat energy is needed to change a substance's temperature. There are two types of specific heat capacity to consider: at constant volume \(c_v\) and at constant pressure \(c_p\).

: This describes the heat required to raise the temperature of a unit mass by one degree Celsius, without changing the volume. In the exercise, the value \(0.177 \text{ cal/g°C}\) was used for calculations involving constant volume.
: Conversely, this is the heat required at constant pressure, where the gas can expand or contract. For nitrogen gas, it was \(0.248 \text{ cal/g°C}\).

These values were crucial for figuring out both the internal energy change and the work done by the gas in different conditions.
Ideal Gas Law
The Ideal Gas Law is a simplified equation of state for a gas, expressed as:\[ PV = nRT \]where \(P\) is pressure, \(V\) is volume, \(n\) is the amount of substance in moles, \(R\) is the gas constant, and \(T\) is temperature.

While it wasn’t directly calculated here, this law helps to understand the behavior of gases under various conditions. For example, it can help predict how a gas's volume changes with pressure and temperature. During the constant pressure process from our exercise, the gas’s volume expanded as it heated, tying in with this concept. Ideal gases, like nitrogen, follow the law under a range of conditions, linking back to the calculations and explanations provided in the thermodynamics context.

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Most popular questions from this chapter

To determine the specific heat of an oil, an electrical heating coil is placed in a calorimeter with \(380 \mathrm{~g}\) of the oil at \(10{ }^{\circ} \mathrm{C}\). The coil consumes energy (and gives off heat) at the rate of \(84 \mathrm{~W}\). After \(3.0 \mathrm{~min}\), the oil temperature is \(40^{\circ} \mathrm{C}\). If the water equivalent of the calorimeter and coil is \(20 \mathrm{~g}\), What is the specific heat of the oil?

A cylinder of ideal gas is closed by an \(8.00 \mathrm{~kg}\) movable piston \(\left(\right.\) area \(\left.=60.0 \mathrm{~cm}^{2}\right)\) as illustrated in Fig. 20-5. Atmospheric pressure is \(100 \mathrm{kPa}\). When the gas is heated from \(30.0{ }^{\circ} \mathrm{C}\) to \(100.0{ }^{\circ} \mathrm{C}\), the piston rises \(20.0 \mathrm{~cm}\). The piston is then fastened in place, and the gas is cooled back to \(30.0{ }^{\circ} \mathrm{C}\). Calling \(\Delta Q_{1}\) the heat added to the gas in the heating process, and \(\Delta Q_{2}\) the heat lost during cooling, find the difference between \(\Delta Q_{1}\) and \(\Delta Q_{2}\). During the heating process, the internal energy changed by \(\Delta U_{1}\), and an amount of work \(\Delta W_{1}\) was done. The absolute pressure of the gas was $$\begin{array}{c} P=\frac{m g}{A}+P_{A} \\ P=\frac{(8.00)(9.81) \mathrm{N}}{60.0 \times 10^{-4} \mathrm{~m}^{2}}+1.00 \times 10^{5} \mathrm{~N} / \mathrm{m}^{2}=1.13 \times 10^{5} \mathrm{~N} / \mathrm{m}^{2} \end{array}$$ $$\text { Therefore, } \begin{aligned} \Delta Q_{1} &=\Delta U_{1}+\Delta W_{1}=\Delta U_{1}+P \Delta V \\ &=\Delta U_{1}+\left(1.13 \times 10^{5} \mathrm{~N} / \mathrm{m}^{2}\right)\left(0.200 \times 60.0 \times 10^{-4} \mathrm{~m}^{3}\right)=\Delta U_{1}+136 \mathrm{~J} \end{aligned}$$ During the cooling process, \(\Delta W=0\) and so (since \(\Delta Q_{2}\) is heat lost) $$-\Delta Q_{2}=\Delta U_{2}$$ But the ideal gas returns to its original temperature, and so its internal energy is the same as at the start. Therefore \(\Delta U_{2}=-\Delta U_{1}\), or \(\Delta Q_{2}=\Delta U_{1} .\) It follows that \(\Delta Q_{1}\) exceeds \(\Delta Q_{2}\) by \(136 \mathrm{~J}=32.5\) cal.

How many joules of heat per hour are produced in a motor that is \(75.0\) percent efficient and requires \(0.250\) hp to run it?

Twenty cubic centimeters of monatomic gas at \(12^{\circ} \mathrm{C}\) and \(100 \mathrm{kPa}\) is suddenly (and adiabatically) compressed to \(0.50 \mathrm{~cm}^{3}\). Assume that we are dealing with an ideal gas. What are its new pressure and temperature? For an adiabatic change involving an ideal gas, \(P_{1} V_{1}^{\gamma}=P_{2} V_{2}^{\gamma}\) where \(\gamma=1.67\) for a monatomic gas. Hence, $$P_{2}=P_{1}\left(\frac{V_{1}}{V_{2}}\right)^{\gamma}=\left(1.00 \times 10^{5} \mathrm{~N} / \mathrm{m}^{2}\right)\left(\frac{20}{0.50}\right)^{1.67}=4.74 \times 10^{7} \mathrm{~N} / \mathrm{m}^{2}=47 \mathrm{MPa}$$ To find the final temperature, we could use \(P_{1} V_{1} / T_{1}=P_{2} V_{2} / T_{2}\). Instead, let us use $$T_{1} V_{1}^{\gamma-1}=T_{2} V_{2}^{\gamma-1}$$ or $$T_{2}=T_{1}\left(\frac{V_{1}}{V_{2}}\right)^{\gamma-1}=(285 \mathrm{~K})\left(\frac{20}{0.50}\right)^{0.67}=(285 \mathrm{~K})(11.8)=3.4 \times 10^{3} \mathrm{~K}$$ As a check, $$ \begin{array}{c} \frac{P_{1} V_{1}}{T_{1}}=\frac{P_{2} V_{2}}{T_{2}} \\ \frac{\left(1 \times 10^{5} \mathrm{~N} / \mathrm{m}^{2}\right)\left(20 \mathrm{~cm}^{3}\right)}{285 \mathrm{~K}}=\frac{\left(4.74 \times 10^{7} \mathrm{~N} / \mathrm{m}^{2}\right)\left(0.50 \mathrm{~cm}^{3}\right)}{3370 \mathrm{~K}} \\ 7000=7000 \swarrow \end{array} $$

A 70 -g metal block moving at \(200 \mathrm{~cm} /\) s slides across a tabletop a distance of \(83 \mathrm{~cm}\) before it comes to rest. Assuming 75 percent of the thermal energy developed by friction goes into the block, how much does the temperature of the block rise? For the metal, \(c=0.106 \mathrm{cal} / \mathrm{g} \cdot{ }^{\circ} \mathrm{C}\).

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