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Modern Engineering Thermodynamics

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534 CHAPTER 13: Vapor and Gas Power Cycles<br />

user’s electrical bill (like wind power devices today). If 100<br />

million people exercised for 15 min every day of the year at a<br />

power level of 100. W each, how many barrels of crude oil<br />

(at 5.80 × 10 6 Btu per barrel) and how many tons of coal<br />

(at 26.0 × 10 6 Btu per ton) could be saved annually?<br />

Computer Problems<br />

The following computer programming assignments are designed to<br />

be carried out on any personal computer using a spreadsheet or<br />

equation solver. They are meant to be exercises in the manipulation<br />

of some of the basic formulae of this chapter. They may be used as<br />

part of a weekly homework assignment.<br />

81. Write a computer program or use an equation solver or<br />

spreadsheet to carry out a parametric study of the isentropic<br />

Rankine cycle with regeneration given in Example 13.6, part<br />

b. Allow the regenerator pressure p 5s to vary from 1.00 to<br />

200. psia (this simulates opening a valve in the regenerator<br />

steam line from the turbine). Maintain the regenerator outlet<br />

state as a saturated liquid (i.e., set h 6 = h f (p 5s )), because if<br />

h 6 < h f (p 5s ), the regenerator is not operating as effectively<br />

as possible; and if h 6 > h f (p 5s ), there will be vapor at the<br />

entrance of the boiler feed pump and its performance will be<br />

seriously degraded.<br />

a. Determine the values of p 5s and mass fraction y that<br />

maximize the cycle efficiency.<br />

b. Produce a plot of cycle efficiency η T and mass fraction y on the<br />

y-axis vs. regenerator pressure p 5s on the x-axis. As part of this<br />

solution, note that, when p 5s is equal to the turbine inlet<br />

pressure (200. psia) or the condenser inlet pressure (1.00 psia),<br />

the regenerator has no effect and the cycle efficiency is the same<br />

as without regeneration (i.e., 29.7%).<br />

82. Repeat Problem 78 using the cycle data from Example 13.6,<br />

except now let the boiler pressure range from 100. to 1000. psia<br />

and keep the regenerator pressure at 25.0% of the boiler<br />

pressure. Plot the cycle efficiency and the regenerator mass<br />

fraction vs. boiler pressure. Does the cycle efficiency have a<br />

maximum value under these conditions?<br />

83. Develop a computer program or use a spreadsheet or equation<br />

solver to calculate the Otto ASC thermal efficiency as the<br />

compression ratio ranges from 1.00 to 12.0 for the following<br />

values of k: 1.40, 1.35, 1.30, 1.25, and 1.20 (note that values of<br />

k less than 1.40 give an approximate hot ASC result). Plot these<br />

results (either manually or with a computer) with the thermal<br />

efficiency on the vertical axis and the compression ratio on the<br />

horizontal axis, using k as a parameter for the family of curves.<br />

Utilize at least 25 points per curve.<br />

84. Develop a computer program or use a spreadsheet or equation<br />

solver to calculate the Diesel cold ASC thermal efficiency as<br />

the compression ratio (CR) ranges from 12.0 to 30.0 for the<br />

following cutoff ratios: 1.50, 2.00, 2.50, 3.00, and 3.50. Plot<br />

these results (either manually or with a computer) with the<br />

thermal efficiency on the vertical axis and the compression<br />

ratio on the horizontal axis, using the cutoff ratio as a<br />

parameter for the family of curves. Utilize at least 25 points<br />

per curve.<br />

85. Develop a computer program or use a spreadsheet or<br />

equation solver that determines the value of the cutoff ratio<br />

that causes the Diesel ASC thermal efficiency to become zero<br />

as the compression ratio ranges from 12.0 to 30.0 for the<br />

following values of k: 1.40, 1.35, 1.30, 1.25, and 1.20. Plot<br />

these results (either manually or with a computer) with the<br />

cutoff ratio on the vertical axis and the compression ratio on<br />

the horizontal axis, using k as a parameter for the family of<br />

curves.

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