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If pure oxygen is compressed such that its density and pressure are \(5 \mathrm{~kg} / \mathrm{m}^{3}\) and \(450 \mathrm{kPa}\), respectively, estimate the temperature of the oxygen.

Short Answer

Expert verified
The temperature of the compressed oxygen is approximately 346.36 K.

Step by step solution

01

Identify the Known Values

We have the density of oxygen, \( \rho = 5 \mathrm{~kg} / \mathrm{m}^{3}\), and the pressure, \( P = 450 \mathrm{kPa} = 450,000 \mathrm{Pa}\). We need to find the temperature, \( T \), of the oxygen.
02

Recall the Ideal Gas Law

The Ideal Gas Law formula is given by \( PV = nRT \), where \( P \) is pressure, \( V \) is volume, \( n \) is the number of moles, \( R \) is the universal gas constant, and \( T \) is temperature. For calculations with density, it's more convenient to use \( P = \rho RT/M \), where \( M \) is the molar mass.
03

Rearrange the Formula

We rearrange the formula to solve for temperature: \[ T = \frac{PM}{\rho R} \]In this equation, \( P \) is pressure, \( M \) is the molar mass of oxygen (about \(32 \mathrm{~g/mol}\) or \(0.032 \mathrm{~kg/mol}\)), \( \rho \) is density, and \( R \) is the specific gas constant (approximately \(8.314 \mathrm{~J/(mol \cdot K)}\)).
04

Substitute the Known Values

By substituting the known values in the formula, we have:\[ T = \frac{450,000 \times 0.032}{5 \times 8.314} \]
05

Calculate the Temperature

Perform the calculation:\[ T = \frac{14400}{41.57} \approx 346.36 \mathrm{~K} \]
06

Interpret the Result

The temperature of the oxygen when compressed to the given density and pressure is approximately \(346.36 \mathrm{~K}\).

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Key Concepts

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

Gas Temperature Estimation
Estimating the temperature of a gas is an essential task in understanding its behavior under different conditions. The temperature of a gas is a measure of the average kinetic energy of its particles. In the context of the Ideal Gas Law, we can use known values like pressure and density to find an unknown temperature. Here's how it works in practice using a specific scenario:When you have pure oxygen with a known pressure (\(450 \mathrm{kPa} = 450,000 \mathrm{Pa}\)) and density (\(5 \mathrm{~kg/m^3}\)), you can determine its temperature using the Ideal Gas Law formula suitably rearranged. The rearranged formula allows the calculation of temperature (\(T\)) from pressure (\(P\)), density (\(\rho\)), and the molar mass of oxygen (\(M\)). Substituting these known values into the formula lets us directly calculate the temperature, yielding a final result of approximately \(346.36 \mathrm{~K}\). This estimation process provides insight into how gas conditions change with pressure and density variations.
Pressure and Density Relationship
Pressure and density have a direct relationship in a gas governed by the Ideal Gas Law. This relationship is essential to understanding how gases behave under varying conditions. When pressure increases at constant temperature and molar mass, density typically increases too.- **Pressure (\(P\)):** This is the force exerted by the gas particles per unit area, measured in Pascals or kilopascals.- **Density (\(\rho\)):** This represents how much mass of the gas is contained within a particular volume, in this case, measured as kilograms per cubic meter.In scenarios where specific values are known, such as a pressure of \(450 \mathrm{kPa}\) and a density of \(5 \mathrm{~kg/m^3}\), one can infer certain properties about the gas. The density increases with pressure under a constant temperature, following the law dynamics. This concept is key in many scientific and engineering applications that require precise gas behavior predictions.
Specific Gas Constant
The specific gas constant (\(R\)) is a crucial term in the Ideal Gas Law, tailoring the law to specific gases. Unlike the universal gas constant, which applies to all gases, the specific gas constant is unique to each one, accounting for differences in molecular composition.- **Definition:** For any gas, the specific gas constant (\(R\)) is calculated as the universal gas constant divided by the molar mass of the gas. It's typically given in units of Joules per kilogram per Kelvin.- **Application:** For pure oxygen, \(R\) is approximately \(259.8 \mathrm{~J/(kg \cdot K)}\), reflecting its molar mass conversion from universal conditions. This parameter helps convert molar-based calculations into mass-based ones, simplifying calculations in practical scenarios.Utilizing this specific gas constant allows for precise gas dynamics understanding, especially when calculating other properties such as temperature, making it an indispensable tool in thermodynamic calculations.

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Most popular questions from this chapter

A liquid with a surface tension of \(0.072 \mathrm{~N} / \mathrm{m}\) is used to form 60 -mm-diameter bubbles in air. What is the difference between the air pressure inside the bubble and the air pressure outside the bubble?

Model tests on a supercavitating torpedo in seawater at \(20^{\circ} \mathrm{C}\) indicate that the minimum pressure, \(p_{\min }\), on the surface of the torpedo is related to the speed, \(V\), of the torpedo by the relation $$ p_{\min }=120-0.402 V^{2} $$ where \(p_{\min }\) is in \(\mathrm{kPa}\) and \(V\) is in \(\mathrm{m} / \mathrm{s}\). What is the minimum torpedo speed required for cavitation to begin on the surface of the torpedo?

A \(2.0-\mathrm{m}^{3}\) volume of pure oxygen at a temperature and pressure of \(20^{\circ} \mathrm{C}\) and \(100 \mathrm{kPa}\), respectively, is expanded to a volume of \(4.0 \mathrm{~m}^{3} .\) (a) What is the pressure in the expanded volume if the expansion process is isentropic? What are the initial and final densities of the gas? (b) What is the pressure in the expanded volume if the expansion process is isothermal? What are the initial and final densities of the gas? (c) For the expansion process described in part (b), what amount of heat must be added to the gas?

The Boeing 787 Dreamliner has a design cruising speed of \(913 \mathrm{~km} / \mathrm{h}\) at an altitude of \(10700 \mathrm{~m}\). Assuming a standard atmosphere, what is the Mach number at which the aircraft flies under cruising conditions? Should the compressibility of air be taken into account in modeling the flight of this aircraft? Explain.

Would you expect that the surface tension of water in contact with air is the same as the surface tension of water in contact with pure oxygen? Explain.

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