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Modern Engineering Thermodynamics

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444 CHAPTER 12: Mixtures of Gases and Vapors<br />

First, the air passes over a cooling coil, where it is cooled below<br />

its dew point temperature and the water condenses out until the<br />

desired humidity ratio is reached. Then, the air is passed over a<br />

reheating coil until its temperature reaches 71.0°F. Determine<br />

a. The amount of water removed per pound of dry air passing<br />

through the device.<br />

b. The heat removed by the cooling coil in Btu/(lbm dry air).<br />

c. The heat added by the reheating coil in Btu/(lbm dry air).<br />

43.* An airstream with a mass flow rate of 2.00 kg/s, a dry bulb<br />

temperature of 10.0°C, and a wet bulb temperature of 8.00°C is<br />

mixed with an airstream having a mass flow rate of 1.00 kg/s, a<br />

dry bulb temperature of 40.0°C, and a wet bulb temperature of<br />

35.0°C. For the resulting mixture, determine the (a) humidity<br />

ratio, (b) psychrometric enthalpy, (c) relative humidity, (d) dry<br />

bulb temperature, (e) wet bulb temperature, and (f) dew point<br />

temperature.<br />

44.* Exactly 200 m 3 /min of air with a dry bulb temperature of<br />

7.00°C and a wet bulb temperature of 5.00°C is continuously<br />

mixed with 500. m 3 /min of air with a dry bulb temperature<br />

of 32.0°C and a relative humidity of 60.0%. The mixing<br />

chamber is at atmospheric pressure and is electrically heated<br />

with a power consumption of 3.00 kW. For the resulting<br />

mixture, determine (a) the dry bulb temperature, (b) the wet<br />

bulb temperature, (c) the dew point temperature, and (d) the<br />

relative humidity.<br />

45.* 100. kg of atmospheric air (whose composition is given in<br />

Example 12.2) is cooled in a 0.500 m 3 constant volume<br />

container to 200. K. Determine the mixture pressure using<br />

Dalton’s compressibility factor. Compare this result with that<br />

obtained by assuming ideal gas (i.e., Z m = 1.00) behavior.<br />

46. Show that the ratio of the Amagat specific volume, v Ai = V Ai /m i ,<br />

to the Dalton specific volume, v Di = V m /m i , of gas i can be<br />

written as v Ai /v Di = Z Ai p Di /Z Di p m .<br />

47.* Atmospheric air, whose composition is given in Example 12.2, is<br />

compressed to 1000. atm at 0.00°C. Determine the density of<br />

the compressed air using Amagat’s compressibility factor and<br />

compare this result with that obtained by assuming ideal gas<br />

(i.e., Z m = 1.00) behavior.<br />

48.* In normal psychrometric analysis at or below atmospheric<br />

pressure, both the air and the water vapor are treated as ideal<br />

gases. However, at high pressures, this assumption is no longer<br />

valid. Determine the relative humidity (ϕ) that results when<br />

10.0 g of water are added to 1.00 kg of dry air at a total pressure<br />

of 10.0 MPa at 350.°C. Assume Amagat’s compressibility factor is<br />

valid here and compare your result with that obtained by<br />

assuming ideal gas behavior.<br />

49.* 0.500 m 3 of a mixture of 35.0% acetylene (C 2 H 2 ), 25.0%<br />

oxygen (O 2 ), 20.0% hydrogen (H 2 ), and 20.0% sulfur dioxide<br />

(SO 2 ) on a mass basis is to be adiabatically compressed in a<br />

piston-cylinder arrangement from 1.00 atm, 20.0°C to 100. atm<br />

and 300.°C.<br />

a. Using Kay’s law, find the final volume of the mixture.<br />

b. Assuming constant specific heats, determine the work<br />

required per unit mass of mixture.<br />

50.* A mixture of 80.0% methane and 20.0% ethane on a molar<br />

basis is contained in an insulated 1.00 m 3 tank at 3.00 MPa<br />

and 50.0°C. An automatic flow control valve opens, causing<br />

the tank pressure to drop quickly to 2.00 MPa before it closes<br />

again.<br />

a. Calculate the mass that escaped from the tank using Kay’s<br />

law.<br />

b. Determine the equilibrium tank temperature when the<br />

control valve closes, assuming that the gas remaining in the<br />

tank underwent a reversible process.<br />

51.* 6.00 kg of hydrogen gas (H 2 ) is mixed with 28.0 kg of nitrogen<br />

gas (N 2 ) and compressed to 40.5 MN/m 2 at 300.°C. At this<br />

state, the specific volume of the mixture is measured and found<br />

to be 0.0160 m 3 /kg. Determine the specific volume of this state<br />

as predicted by each of the following models and calculate the<br />

percent deviation from the measured value.<br />

a. Ideal gas model.<br />

b. Dalton’s law compressibility factor.<br />

c. Amagat’s law compressibility factor.<br />

d. Kay’s law.<br />

52.* Determine the total mixture volume when 1 kgmole each of<br />

hydrogen (H 2 ) and helium (He) gases are mixed at 15.0 atm<br />

and 40.0 K, using<br />

a. Dalton’s law compressibility factor.<br />

b. Amagat’s law compressibility factor.<br />

c. Kay’s law.<br />

d. Which of the three results do you believe is the most<br />

accurate, and why?<br />

Design Problems<br />

The following are open-ended design problems. The objective is to<br />

carry out a preliminary thermal design as indicated. A detailed<br />

design with working drawings is not expected unless otherwise specified.<br />

These problems do not have specific answers, so each student’s<br />

designisunique.<br />

53. Design an electrically driven sling psychrometer to produce the<br />

wet and dry bulb temperatures on digital readouts. The<br />

finished product must cost less than 30.0 h of minimum wage<br />

pay and be battery powered. If possible, fabricate and test your<br />

design. (Suggestion: Try designing around inexpensive, “off the<br />

shelf” components.)<br />

54. Design an apparatus to measure the dew point of an air sample<br />

based on the cooling of a mirrored surface until it fogs. If<br />

possible, build and test this apparatus. (Suggestion: Consider<br />

thermoelectric cooling of a polished metal plate.)<br />

55.* Design a system to remove the respiration carbon dioxide from<br />

inside a spacecraft and replace it with oxygen. Use a living<br />

quarters volume of 10.0 m 3 with the crew generating a<br />

maximum of 2.00 × 10 −5 m 3 /s of CO 2 . Assume the mixture<br />

enters your system at 30.0°C and exits it at 20.0°C. Maintain<br />

the same oxygen partial pressure in your mixture as that in<br />

atmospheric air at 0.1013 MPa and 20.0°C.<br />

56.* Design a system to remove the respiration carbon dioxide<br />

from inside a submarine and replace it with oxygen. The air<br />

volume of the submarine is 1000. m 3 ,andthecrewcan<br />

generate a maximum of 1.30 × 10 −3 m 3 /s of CO 2 .The<br />

submarine must be able to achieve a depth of 300. m. Assume<br />

the air mixture enters your system at 30.0°C and exits at<br />

20.0°C. Maintain the oxygen partial pressure at all times in<br />

your mixture equal to that in atmospheric air at 0.1013 MPa<br />

and 20.0°C.

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