/*! 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 39 On a warm summer day, a large ma... [FREE SOLUTION] | 91Ó°ÊÓ

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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 a temperature of \(26.0^{\circ} \mathrm{C}\) 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 cool- ing for dry, rising air, corresponding to roughly \(1^{\circ} \mathrm{C}\) per 100 \(\mathrm{m}\) of altitude, is called the dry adiabatic lapse rate.)

Short Answer

Expert verified
The air mass cools to approximately 11.7°C.

Step by step solution

01

Understand the Problem

We need to determine the temperature of a rising air mass when it reaches a higher altitude with a given atmospheric pressure and temperature change as an adiabatic process. We're given the initial conditions: atmospheric pressure \( P_1 = 1.01 \times 10^5 \text{ Pa} \) and temperature \( T_1 = 26.0^{\circ} \text{C} \). The final pressure is \( P_2 = 0.850 \times 10^5 \text{ Pa} \). We need to find the final temperature \( T_2 \) given that \( \gamma = 1.40 \).
02

Convert Initial Temperature to Kelvin

We convert the initial temperature from Celsius to Kelvin using the formula: \( T_1(K) = T_1(^{\circ}C) + 273.15 \). Thus, \( T_1 = 26.0 + 273.15 = 299.15 \text{ K} \).
03

Apply Adiabatic Process Formula

For an adiabatic process involving an ideal gas, the relationship between pressure and temperature is given by: \( \frac{T_2}{T_1} = \left( \frac{P_2}{P_1} \right)^\frac{\gamma-1}{\gamma} \). Substitute \( T_1 = 299.15 \text{ K} \), \( P_1 = 1.01 \times 10^5 \text{ Pa} \), \( P_2 = 0.850 \times 10^5 \text{ Pa} \), and \( \gamma = 1.40 \).
04

Calculate Temperature Ratio

Calculate \( \left( \frac{P_2}{P_1} \right)^\frac{\gamma-1}{\gamma} = \left( \frac{0.850 \times 10^5}{1.01 \times 10^5} \right)^\frac{0.40}{1.40} \). Evaluate this expression to find the ratio.
05

Determine Final Temperature

Using the temperature ratio from Step 4, calculate \( T_2 \) by multiplying \( T_1 \) with the ratio: \( T_2 = T_1 \times \text{ratio} \). Perform the multiplication to find \( T_2 \).
06

Convert Final Temperature to Celsius

Once \( T_2 \) is calculated in Kelvin, convert it back to Celsius using \( T_2(^{\circ}C) = T_2(K) - 273.15 \). This will give the final temperature in Celsius.

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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 key principle in thermodynamics that explains the behavior of gases under various conditions. This law combines several fundamental relationships into one simple equation: \[ PV = nRT \] where
  • \( P \) is the pressure of the gas,
  • \( V \) is the volume,
  • \( n \) is the number of moles of gas,
  • \( R \) is the universal gas constant, and
  • \( T \) is the temperature in Kelvin.
This equation tells us how changes in one of these factors can affect the others while keeping the state of the gas consistent. In the context of our exercise, the Ideal Gas Law helps us understand how pressure and temperature interact as a mass of air rises and cools. When an air mass rises, it's subjected to lower atmospheric pressure, causing it to expand and cool in an adiabatic process. Even though the Ideal Gas Law is not directly used in the solution to calculate temperatures in an adiabatic process, it provides foundational knowledge about how gases behave under different conditions.
Dry Adiabatic Lapse Rate
The dry adiabatic lapse rate describes how the temperature of a rising air mass changes as it moves upward through the atmosphere, provided no moisture is present. In an adiabatic process, the heat is transferred internally within the system, meaning no heat is gained or lost to the environment. For dry air, this rate of temperature change is approximately \( 1^{\circ} \text{C} \) per \( 100 \text{ m} \) of elevation gain. This adiabatic cooling happens because the air mass expands as it rises due to decreasing atmospheric pressure, causing its temperature to drop. Understanding this rate is crucial in meteorology and aviation for predicting weather patterns and planning flight paths, as it helps make sense of atmospheric stability and the development of clouds and storms.
Atmospheric Pressure
Atmospheric pressure is the force exerted by the weight of air in the Earth's atmosphere pressing down on a surface. It decreases with altitude as the air becomes less dense. At sea level, standard atmospheric pressure is approximately \( 1.01 \times 10^{5} \text{ Pa} \).In our exercise, atmospheric pressure is a key variable that affects the behavior of the air mass as it rises. As the pressure drops, the air mass expands and cools according to the principles of adiabatic processes. This pressure variation helps us understand the drop in temperature as the air ascends, which is crucial for calculating the new temperature of the air mass at lower pressure levels.
Temperature Conversion
When working with thermodynamic calculations, temperature needs to be in absolute terms, using the Kelvin scale. To convert from Celsius to Kelvin, add 273.15 to the Celsius temperature: \[ T(K) = T(^{\circ}C) + 273.15 \] This conversion is crucial because physical laws like the Ideal Gas Law require temperatures in Kelvin for correct results. Kelvin starts at absolute zero, the theoretical point where all molecular motion ceases, making it ideal for scientific calculations. In our problem, converting temperatures is essential because we begin with an initial air temperature in Celsius that must be used in thermodynamic formulas in Kelvin. After completing calculations, we often convert back to Celsius for easier interpretation and communication of results, especially when reporting temperature changes or conditions experienced by humans.

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Most popular questions from this chapter

A Thermodynamic \(\mathbf{P} \mathbf{r} \mathbf{o}-\) cess In an Insect. The Africanbombardier beetle Stenaptinus insignis can emit a jet of defensive spray from the movable tip of its abdomen (Fig, 19.32\()\) . The beetle's body has reservoirs of two different chemicals; when the beetle is disturbed, these chemicals are combined in a reaction chamber, producing compound that is warmed from \(20^{\circ} \mathrm{C}\) to \(100^{\circ} \mathrm{C}\) by the heat of reaction. The high pressure produced allows the compound to be sprayed out at speeds up to 19 \(\mathrm{m} / \mathrm{s}(68 \mathrm{km} / \mathrm{h})\) , scaring away predators of all kinds. (The beetle shown in the figure is 2 \(\mathrm{cm}\) long.) Calculate the heat of reaction of the two chemicals (in J/kg). Assume that the specific heat capacity of the two chemicall and the spray is the same as that of water, \(4.19 \times 10^{3} \mathrm{J} / \mathrm{kg} \cdot \mathrm{K}\) , and that the initial temperature of the chemicals is \(20^{\circ} \mathrm{C}\) .

A monatomic ideal gas that is initially at a pressure of \(1.50 \times 10^{5} \mathrm{Pa}\) and has a volume of 0.0800 \(\mathrm{m}^{3}\) is compressed adiabatically to a volume of \(0.0400 \mathrm{m}^{3} .\) (a) What is the final pressure? (b) How much work is done by the gas?(c) What is the ratio of the final temperature of the gas to its initial temperature? Is the gas heated or cooled by this compression?

Oscillations of a Piston. A vertical cylinder of radins \(r\) contains a quantity of ideal gas and is fitted with a piston with mass \(m\) that is free to move (Fig. 19.34\()\) . The piston and the walls of the cylinder are frictionless and the entire cylinder is placed in aconstant-temperature bath. The outside air pressure is \(p_{0}\) . In equilibrium, the piston sits at a height \(h\) above the bottom of the cylinder. (a) Find the absolute pressure of the gas trapped below the piston when in equilibrium. (b) The piston is pulled up by a small distance and released. Find the net force acting on the piston when its base is a distance \(h+y\) above the bottom of the cylinder, where \(y\) is much less than \(h\) (c) After the piston is displaced from equilibrium and released, it oscillates up and down. Find the frequency of nthese small oscillations. If the displacement is not small, are the oscillations simple harmonic? How can you tell?

Two moles of an ideal gas are heated at constant pressure from \(T=27^{\circ} \mathrm{C}\) to \(T=107^{\circ} \mathrm{C}\) (a) Draw a \(p V\) -diagram for this process. (b) Calculate the work done by the gas.

The engine of a Ferrari \(\mathrm{F} 355 \mathrm{FI}\) sports car takes in air at \(20.0^{\circ} \mathrm{C}\) and 1.00 \(\mathrm{atm}\) and compresses it adiabatically to 0.0900 times the original volume. The air may be treated as an ideal gas with \(\gamma=1.40 .\) (a) Draw a \(p V\) -diagram for this process. (b) Find the final temperature and pressure.

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