/*! 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 20 A stream of air at \(77^{\circ} ... [FREE SOLUTION] | 91Ó°ÊÓ

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A stream of air at \(77^{\circ} \mathrm{F}\) and 1.2 atm absolute flowing at a rate of \(225 \mathrm{ft}^{3} / \mathrm{h}\) is blown through ducts that pass through the interior of a large industrial motor. The air emerges at \(500^{\circ} \mathrm{F}\). Calculate the rate at which the air is removing heat generated by the motor. What assumption have you made about the pressure dependence of the specific enthalpy of air?

Short Answer

Expert verified
The rate at which the air is removing heat generated by the motor is 1713 Btu/h. The assumption made about the pressure dependence of the specific enthalpy of air is that it is negligible at these pressures and temperatures.

Step by step solution

01

- Conversion of temperatures to Rankine

To make the computations, convert all the temperatures from Fahrenheit to Rankine. Utilize the conversion formula \( R = F + 459.67 \). Hence, the inlet temperature is \(77^{\circ}F + 459.67 = 536.67^{\circ}R\) and the outlet temperature is \(500^{\circ}F + 459.67 = 959.67^{\circ}R\).
02

- Calculation of enthalpy

To calculate the enthalpy, use the formula \( \Delta h = cp \Delta T \), where \(\Delta h\) is the change in enthalpy, \(cp\) is the specific heat capacity at constant pressure, and \(\Delta T\) is the difference in temperature. For standard air, \(cp\) is approximately 0.24 Btu/lb°F. Therefore, \(\Delta h = 0.24 (959.67 - 536.67) = 101.52 Btu/lb\).
03

- Determining the flow rate

The properties of standard air at 60°F and 14.696 psia can be found in standard tables. The density of air is \(0.075 lb/ft^3\), therefore the mass flow rate can be calculated as \(225 ft^3/h * 0.075 lb/ft^3 = 16.875 lb/h\).
04

- Calculation of heat removal rate

Calculate the heat removal rate using the formula \( Q = \dot{m} \Delta h \), where \( Q \) is the heat removal rate and \( \dot{m} \) is the mass flow rate. This gives you \( Q = 16.875 lb/h * 101.52 Btu/lb = 1713 Btu/h \).

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Key Concepts

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

Specific Heat Capacity
Specific heat capacity is a property of a material that tells you how much heat energy is needed to change its temperature. For air, the specific heat capacity is the amount of heat required to raise the temperature of one pound of air by one degree Fahrenheit when pressure remains constant.
In our enthalpy calculations, we denote specific heat capacity with the symbol \( c_p \). This is because we're assuming pressure remains constant while air flows through the ducts. The value for \( c_p \) for air, at standard conditions, is roughly 0.24 Btu/lb°F.
Understanding specific heat capacity is crucial because it is part of the formula used to calculate the change in enthalpy, \( \Delta h = c_p \Delta T \). This tells us how much heat is absorbed or released as the air's temperature changes as a result of the motor's heat.
  • Is material-specific
  • Helps compute energy changes
  • Involves in constant pressure conditions
Temperature Conversion
Temperature conversions are vital when working with thermodynamic calculations, especially in contexts like enthalpy calculations that require consistent units.
In the given exercise, we initially have temperatures in degrees Fahrenheit and we need to convert these to Rankine for our calculations. This is because Rankine is the absolute temperature scale used in this kind of thermodynamic problem involving British Thermal Units (BTU).
We use the conversion formula \( R = F + 459.67 \) to change Fahrenheit to Rankine. This transition standardizes the temperature values and allows for the direct application of enthalpy formulas.
  • Converts Fahrenheit (°F) to Rankine (°R).
  • Ensures compatibility with the BTU unit of energy.
  • Simplifies thermodynamic equations.
Heat Transfer
Heat transfer dictates how thermal energy moves from one place to another. In our scenario, the stream of air moves heat from the motor's interior through the ducts, cooling the motor.
The calculation for heat transfer relies on mass flow rate and specific enthalpy change. It follows the formula \( Q = \dot{m} \Delta h \). Here, \( Q \) is the rate of heat removal, \( \dot{m} \) represents the mass flow rate of the air, and \( \Delta h \) is the change in enthalpy.
This setup assumes the motor's heat is being transferred to the air efficiently, indicated by consistent pressure (hence we use specific heat at constant pressure). Through this assumption, enthalpy is considered only dependent on temperature change. It's also important to note that efficient heat transfer ensures the motor works optimally without overheating.
  • Involves moving heat energy efficiently.
  • Calculated using mass flow and enthalpy change.
  • Requires assumptions about pressure dependency.

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Most popular questions from this chapter

Propane is to be burned with \(25.0 \%\) excess air. Before entering the furnace, the air is preheated from \(32^{\circ} \mathrm{F}\) to \(575^{\circ} \mathrm{F}\) (a) At what rate (B tu/h) must heat be transferred to the air if the feed rate of propane is \(1.35 \times 10^{5}\) SCFH (ft \(^{3} / \mathrm{h}\) at \(\mathrm{STP}\) )? (b) The stack gas leaves the furnace at \(855^{\circ} \mathrm{F}\). How is the air likely to be preheated?

A natural gas containing 95 mole \(\%\) methane and the balance ethane is burned with \(20.0 \%\) excess air. The stack gas, which contains no unburned hydrocarbons or carbon monoxide, leaves the furnace at \(900^{\circ} \mathrm{C}\) and \(1.2 \mathrm{atm}\) and passes through a heat exchanger. The air on its way to the furnace also passes through the heat exchanger, entering it at \(20^{\circ} \mathrm{C}\) and leaving it at \(245^{\circ} \mathrm{C}\). (a) Taking as a basis \(100 \mathrm{mol} / \mathrm{s}\) of the natural gas fed to the furnace, calculate the required molar flow rate of air, the molar flow rate and composition of the stack gas, the required rate of heat transfer in the preheater, \(\dot{Q}\) (write an energy balance on the air), and the temperature at which the stack gas leaves the preheater (write an energy balance on the stack gas). Note: The problem statement does not give you the fuel feed temperature. Make a reasonable assumption, and state why your final results should be nearly independent of what you assume. (b) What would \(\dot{Q}\) be if the actual feed rate of the natural gas were 350 SCMH [standard cubic meters per hour, \(\left.\mathrm{m}^{3}(\mathrm{STP}) / \mathrm{h}\right] ?\) Scale up the flowchart of Part (a) rather than repeating the entire calculation.

Estimate the heat of vaporization of diethyl ether at its normal boiling point using Trouton's rule and Chen's rule and compare the results with a tabulated value of this quantity. Calculate the percentage error that results from using each estimation. Then estimate \(\Delta \hat{H}_{\mathrm{v}}\) at \(100^{\circ} \mathrm{C}\) using Watson's correlation.

The heat capacity at constant pressure of a gas is determined experimentally at several temperatures, with the following results: $$\begin{array}{|l|c|c|c|c|c|c|c|} \hline T\left(^{\circ} \mathrm{C}\right) & 0 & 100 & 200 & 300 & 400 & 500 & 600 \\ \hline C_{p}\left[\mathrm{J} /\left(\mathrm{mol} \cdot^{\circ} \mathrm{C}\right)\right] & 33.5 & 35.1 & 36.7 & 38.4 & 40.2 & 42.0 & 43.9 \\ \hline \end{array}$$ (a) Calculate the heat (kW) required to raise 150 mol/s of the gas from 0^ C to 600^'C, using Simpson's rule (Appendix A.3) to integrate the tabulated heat capacities. (b) Use the method of least squares (Appendix A.1) to derive a linear expression for \(C_{p}(T)\) in the range \(0^{\circ} \mathrm{C}\) to \(600^{\circ} \mathrm{C},\) and use this expression to estimate once again the heat ( \(\mathrm{kW}\) ) required to raise 150 mol/s of the gas from 0 ^ C to 600^'C. If the estimates differ, in which one would you have more confidence, and why?

As part of a design calculation, you must evaluate an enthalpy change for an obscure organic vapor that is to be cooled from \(1800^{\circ} \mathrm{C}\) to \(150^{\circ} \mathrm{C}\) in a heat exchanger. You search through all the standard references for tabulated enthalpy or heat capacity data for the vapor but have no luck at all, until you finally stumble on an article in the May 1922 Antarctican Journal of Obscure Organic Vapors that contains a plot of \(C_{p}\left[\operatorname{cal} /\left(\mathrm{g} \cdot^{\cdot} \mathrm{C}\right)\right]\) on a logarithmic scale versus \(\left[T\left(^{\circ} \mathrm{C}\right)\right]^{1 / 2}\) on a linear scale. The plot is a straight line through the points \(\left(C_{p}=0.329, T^{1 / 2}=7.1\right)\) and \(\left(C_{p}=0.533, T^{1 / 2}=17.3\right)\) (a) Derive an equation for \(C_{p}\) as a function of \(T.\) (b) Suppose the relationship of Part (a) turns out to be $$ C_{p}=0.235 \exp \left[0.0473 T^{1 / 2}\right] $$ and that you wish to evaluate $$ \Delta \hat{H}(\mathrm{cal} / \mathrm{g})=\int_{1800 \mathrm{c}}^{150^{\circ} \mathrm{C}} C_{p} d T $$ First perform the integration analytically, using a table of integrals if necessary; then write a spreadsheet or computer program to do it using Simpson's rule (Appendix A.3). Have the program evaluate \(C_{p}\) at 11 equally spaced points from \(150^{\circ} \mathrm{C}\) to \(1800^{\circ} \mathrm{C}\), estimate and print the value of \(\Delta H,\) and repeat the calculation using 101 points. What can you conclude about the accuracy of the numerical calculation?

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