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Modern Engineering Thermodynamics

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Problems 527<br />

7. The thermal efficiency of a Stirling cold ASC external combustion engine is<br />

ðη T Þ Stirling<br />

= 1 − T L /T H = 1 − T 2 /T 1 = 1 − T 3 /T 4<br />

cold ASC<br />

8. The thermal efficiency of an Ericsson cold ASC external combustion engine is<br />

ðη T Þ Ericsson<br />

= 1 − T L /T H = 1 − T 2 /T 1 = 1 − T 3 /T 4<br />

cold ASC<br />

9. The thermal efficiency of a Lenoir cold ASC internal combustion engine is<br />

ðη T Þ Lenoir<br />

= 1 − kT 3 ðCR − 1Þ/ ðT 1 − T 4 Þ<br />

cold ASC<br />

10. The thermal efficiency of a Brayton cold ASC external combustion engine is<br />

ðη T Þ Brayton<br />

= 1 − T 3 /T 4s = 1 − PR ð1−kÞ/k = 1 − CR 1−k<br />

cold ASC<br />

11. The thermal efficiency of an Otto cold ASC internal combustion engine is<br />

ðη T Þ Otto<br />

= 1 − T 3 /T 4s = 1 − PR ð1−kÞ/k = 1 − CR 1−k<br />

cold ASC<br />

12. The thermal efficiency of a Diesel cold ASC internal combustion engine is<br />

ðη T Þ Diesel<br />

= 1 − CR1−k ðCO k − 1Þ<br />

kðCO − 1Þ<br />

cold ASC<br />

where CO is the cutoff ratio of the engine.<br />

13. The indicated cold ASC power output of either an Otto or Diesel cycle engine is<br />

ð<br />

ð _W 1 Þ out =<br />

η TÞ ASC<br />

_Q/ _m ðDNp fuel 1 /CÞ<br />

ðA/FÞðRT 1 ÞðCR − 1Þ<br />

where D is the engine’s total displacement, N is the engine speed in revolutions per time, C is the number<br />

of crankshaft revolutions per power stroke, and A/F is the air/fuel ratio of the engine.<br />

14. The thermal efficiency of an Atkinson cold ASC internal combustion engine is<br />

ðη T Þ Atkinson<br />

cold ASC<br />

kðER − CRÞ<br />

= 1 −<br />

ER k − CR k<br />

where ER is the isentropic expansion ratio v 2s /v 1 and CR is the isentropic compression ratio v 3 /v 4s .<br />

15. The actual thermal efficiency of any of the cycles discussed in this chapter is<br />

where η m is the mechanical efficiency of the engine.<br />

ðη T Þ actual = ðη m Þðη T Þ ASC<br />

Problems (* indicates problems in SI units)<br />

1. The duty of a 1718 Newcomen engine was found to be 4.30<br />

million. Determine its thermal efficiency (%).<br />

2. In 1767, John Smeaton measured the performance of a<br />

particularly efficient Newcomen engine that had a 42.0-inch<br />

diameter piston and found that it produced 16.7 net horsepower<br />

with a duty of 7.44 million. Determine (a) the thermal efficiency<br />

of the engine and (b) the boiler heat input rate.<br />

3. In 1767 John Smeaton measured the performance of a<br />

Newcomen engine with a 60.0-inch diameter piston and found<br />

that it produced 40.8 net horsepower with a duty of 5.88<br />

million. Determine (a) the thermal efficiency of this engine and<br />

(b) its boiler heat input rate.<br />

4. In 1767, John Smeaton measured the performance of a<br />

Newcomen engine with a 75.0-inch diameter piston and found<br />

that it produced 37.6 net horsepower with a duty of 4.59<br />

million. Determine (a) the thermal efficiency of this engine and<br />

(b) the boiler heat input rate.<br />

5. In 1772, John Smeaton used the results of his tests on various<br />

existing Newcomen cycle engines to design and build his own<br />

atmospheric steam engine. It had a 52.0-inch diameter piston<br />

with a 7.0 ft stroke and operated at 12.5 strokes per minute<br />

with a mean effective pressure of 7.50 lbf/in 2 . It produced a<br />

remarkably high duty of 9.45 million. Determine the (a)<br />

thermal efficiency, (b) the horsepower output, and (c) the boiler

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