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Natural gas at \(23^{\circ} \mathrm{C}, 1\) bar enters a furnace with the following molar analysis: \(40 \%\) propane \(\left(\mathrm{C}_{3} \mathrm{H}_{8}\right), 40 \%\) ethane \(\left(\mathrm{C}_{2} \mathrm{H}_{6}\right), 20 \%\) methane \(\left(\mathrm{CH}_{4}\right)\). Determine (a) the analysis in terms of mass fractions. (b) the partial pressure of each component, in bar. (c) the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\), for a volumetric flow rate of \(20 \mathrm{~m}^{3} / \mathrm{s}\).

Short Answer

Expert verified
Mass fractions are 0.5366 for propane, 0.3659 for ethane, and 0.0976 for methane. Partial pressures are 0.4 bar for propane, 0.4 bar for ethane, and 0.2 bar for methane. Mass flow rate is 29.87 kg/s.

Step by step solution

01

- Calculate Molar Masses

First, find the molar masses of each gas. For propane (\text{C}_3\text{H}_8): \[ \text{C}_3\text{H}_8 = 3 \times 12 + 8 \times 1 = 44 \text{ g/mol} \] For ethane (\text{C}_2\text{H}_6): \[ \text{C}_2\text{H}_6 = 2 \times 12 + 6 \times 1 = 30 \text{ g/mol} \] For methane (\text{CH}_4): \[ \text{CH}_4 = 12 + 4 \times 1 = 16 \text{ g/mol} \]
02

- Determine Mass Fractions

Use the molar fractions to find the mass fraction of each component. For propane: \[ \text{Mass fraction of propane} = \frac{40 \times 44}{40 \times 44 + 40 \times 30 + 20 \times 16} \] For ethane: \[ \text{Mass fraction of ethane} = \frac{40 \times 30}{40 \times 44 + 40 \times 30 + 20 \times 16} \] For methane: \[ \text{Mass fraction of methane} = \frac{20 \times 16}{40 \times 44 + 40 \times 30 + 20 \times 16} \] Simplifying the denominators: \[ (\text{denominator}) = 40 \times 44 + 40 \times 30 + 20 \times 16 = 1760 + 1200 + 320 = 3280 \text{ g} \]
03

- Calculate Mass Fractions

Now, calculate the mass fraction of each component. For propane: \[ \text{Mass fraction of propane} = \frac{40 \times 44}{3280} = \frac{1760}{3280} = 0.5366 \] For ethane: \[ \text{Mass fraction of ethane} = \frac{40 \times 30}{3280} = \frac{1200}{3280} = 0.3659 \] For methane: \[ \text{Mass fraction of methane} = \frac{20 \times 16}{3280} = \frac{320}{3280} = 0.0976 \]
04

- Determine Partial Pressures

Given the total pressure is 1 bar, the partial pressure of each gas is calculated using its mole fraction. For propane: \[ \text{Partial pressure of propane} = 0.4 \times 1 \text{ bar} = 0.4 \text{ bar} \] For ethane: \[ \text{Partial pressure of ethane} = 0.4 \times 1 \text{ bar} = 0.4 \text{ bar} \] For methane: \[ \text{Partial pressure of methane} = 0.2 \times 1 \text{ bar} = 0.2 \text{ bar} \]
05

- Determine Mass Flow Rate

Use the ideal gas law to determine the total mass flow rate. The volume flow rate is given as \(20 \text{ m}^3/\text{s}\), and the molar mass of the mixture is the weighted average: \[ \text{Molar mass of mixture} = 0.4 \times 44 + 0.4 \times 30 + 0.2 \times 16 = 36.8 \text{ g/mol}\] Convert the flow rate to moles per second: \[ \text{n} = \frac{PV}{RT} \] Given: \(P = 1 \text{ bar} = 10^5 \text{ Pa}\), \(V = 20 \text{ m}^3/\text{s}\), \(R = 8.314 \text{ J/mol K}\), \(T = (23+273)K = 296K\), \[ \text{n} = \frac{10^5 \times 20}{8.314 \times 296} = 811.8 \text{ moles/s} \] Finally, calculate the mass flow rate: \[ \text{Mass flow rate} = 811.8 \times 36.8 \text{ g/s} = 2.987 \times 10^4 \text{ g/s} = 29.87 \text{ kg/s} \]

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Key Concepts

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

Molar Mass Calculation
Knowing the molar mass of each gas component in a mixture is crucial for further calculations. The molar mass (M) is the mass of one mole of a substance. It can be derived from the periodic table, where the atomic masses of the elements are listed. For example:
- For propane (C₃H₈):
\[ M_{C₃H₈} = (3 \times 12 \text{ g/mol}) + (8 \times 1 \text{ g/mol}) = 44 \text{ g/mol} \]
- For ethane (C₂H₆):
\[ M_{C₂H₆} = (2 \times 12 \text{ g/mol}) + (6 \times 1 \text{ g/mol}) = 30 \text{ g/mol} \]
- For methane (CH₄):
\[ M_{CH₄} = 12 \text{ g/mol} + (4 \times 1 \text{ g/mol}) = 16 \text{ g/mol} \]
Understanding these values allows us to convert mole fractions into mass fractions and proceed with other thermodynamic calculations.
Mass Fraction Determination
The mass fraction represents the ratio of the mass of a specific component to the total mass of the mixture. First, convert molar fractions to mass fractions using the molar masses calculated. This is done by multiplying each component's molar fraction by its molar mass and then dividing by the total mass of the mixture.

For propane:
\[ \text{Mass fraction of propane} = \frac{40 \times 44}{40 \times 44 + 40 \times 30 + 20 \times 16} = \frac{40 \times 44}{3280} = 0.5366 \]
For ethane:
\[ \text{Mass fraction of ethane} = \frac{40 \times 30}{3280} = 0.3659 \]
For methane:
\[ \text{Mass fraction of methane} = \frac{20 \times 16}{3280} = 0.0976 \]
These fractions reflect the proportion of each gas by weight in the mixture.
Partial Pressure
Partial pressure is the pressure a gas in a mixture would exert if it alone occupied the entire volume. Given the total pressure of the gas mixture, each component's partial pressure can be found by multiplying its mole fraction by the total pressure. With a total pressure of 1 bar, the partial pressures are:
- For propane:
\[ \text{Partial pressure of propane} = 0.4 \times 1 \text{ bar} = 0.4 \text{ bar} \]
- For ethane:
\[ \text{Partial pressure of ethane} = 0.4 \times 1 \text{ bar} = 0.4 \text{ bar} \]
- For methane:
\[ \text{Partial pressure of methane} = 0.2 \times 1 \text{ bar} = 0.2 \text{ bar} \]
These values are essential for various applications, including gas law equations and chemical reactions involving gases.
Ideal Gas Law
The ideal gas law relates the pressure (P), volume (V), and temperature (T) of an ideal gas with its amount in moles (n) through the equation:
\[ PV = nRT \]
where R is the universal gas constant (8.314 \text{ J/(mol K)} ). To find the number of moles in a gas flow, use:
\[ n = \frac{PV}{RT} \]
Given: \[ P = 1 \text{ bar} = 10^5 \text{ Pa}, \ V = 20 \text{ m}^3/\text{s}, \ T = 296 \text{ K} \]
The calculation becomes:
\[ n = \frac{10^5 \times 20}{8.314 \times 296} = 811.8 \text{ moles/s} \]
This formula is fundamental for converting between different gas properties and conditions.
Mass Flow Rate Calculation
The mass flow rate is critical in determining how much mass of a gas passes through a point per unit time. To calculate it from a known volumetric flow rate, use the formula:
\[ \text{Mass flow rate} = n \times \text{Molar mass} \]
With the molar mass of the gas mixture calculated as:
\[ \text{Molar mass of mixture} = 0.4 \times 44 + 0.4 \times 30 + 0.2 \times 16 = 36.8 \text{ g/mol} \]
And the number of moles per second (n) using the ideal gas law:
\[ n = 811.8 \text{ moles/s} \]
Finally, the mass flow rate is:
\[ \text{Mass flow rate} = 811.8 \times 36.8 = 2.987 \times 10^4 \text{ g/s} = 29.87 \text{ kg/s} \]
Understanding this process allows for accurate measurement of gas movement in industrial and laboratory settings.

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Most popular questions from this chapter

Air at \(35^{\circ} \mathrm{C}, 1\) bar, and \(10 \%\) relative humidity enters an evaporative cooler operating at steady state. The volumetric flow rate of the incoming air is \(50 \mathrm{~m}^{3} / \mathrm{min}\). Liquid water at \(20^{\circ} \mathrm{C}\) enters the cooler and fully evaporates. Moist air exits the cooler at \(25^{\circ} \mathrm{C}, 1\) bar. If there is no significant heat transfer between the device and its surroundings, determine (a) the rate at which liquid enters, in \(\mathrm{kg} / \mathrm{min}\). (b) the relative humidity at the exit. (c) the rate of exergy destruction, in \(\mathrm{kJ} / \mathrm{min}\), for \(T_{0}=20^{\circ} \mathrm{C}\). Neglect kinetic and potential energy effects.

A device is being designed to separate into components a natural gas consisting of \(\mathrm{CH}_{4}\) and \(\mathrm{C}_{2} \mathrm{H}_{6}\) in which the mole fraction of \(\mathrm{C}_{2} \mathrm{H}_{6}\), denoted by \(y\), may vary from \(0.05\) to \(0.50\). The device will receive natural gas at \(20^{\circ} \mathrm{C}, 1 \mathrm{~atm}\) with a volumetric flow rate of \(100 \mathrm{~m}^{3} / \mathrm{s}\). Separate streams of \(\mathrm{CH}_{4}\) and \(\mathrm{C}_{2} \mathrm{H}_{6}\) will exit, each at \(20^{\circ} \mathrm{C}, 1 \mathrm{~atm}\). Heat transfer between the device and its surroundings occurs at \(20^{\circ} \mathrm{C}\). Ignoring kinetic and potential energy effects, plot versus \(y\) the minimum theoretical work input required at steady state, in \(\mathrm{kW}\).

Answer the following questions involving a mixture of two gases: (a) When would the analysis of the mixture in terms of mass fractions be identical to the analysis in terms of mole fractions? (b) When would the apparent molecular weight of the mixture equal the average of the molecular weights of the two gases?

Moist air at \(20^{\circ} \mathrm{C}, 1 \mathrm{~atm}, 43 \%\) relative humidity and a volumetric flow rate of \(900 \mathrm{~m}^{3} / \mathrm{h}\) enters a control volume at steady state and flows along a surface maintained at \(65^{\circ} \mathrm{C}\), through which heat transfer occurs. Liquid water at \(20^{\circ} \mathrm{C}\) is injected at a rate of \(5 \mathrm{~kg} / \mathrm{h}\) and evaporates into the flowing stream. For the control volume, \(\dot{W}_{\mathrm{cv}}=0\), and kinetic and potential energy effects are negligible. Moist air exits at \(32^{\circ} \mathrm{C}, 1 \mathrm{~atm}\). Determine (a) the rate of heat transfer, in \(\mathrm{kW}\). (b) the rate of entropy production, in \(\mathrm{kW} / \mathrm{K}\).

Atmospheric air having dry-bulb and wet-bulb temperatures of 33 and \(29^{\circ} \mathrm{C}\), respectively, enters a well-insulated chamber operating at steady state and mixes with air entering with dry-bulb and wet- bulb temperatures of 16 and \(12^{\circ} \mathrm{C}\), respectively. The volumetric flow rate of the lower temperature stream is three times that of the other stream. A single mixed stream exits. The pressure is constant throughout at 1 atm. Neglecting kinetic and potential energy effects, determine for the exiting stream (a) the relative humidity. (b) the temperature, in \({ }^{\circ} \mathrm{C}\).

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