Optimum Power Boosting of Gas Turbine Cycles With Compressor Inlet Air Refrigeration
Author:
Affiliation:
1. Ecole Nationale Polytechnique, B. P. 182 Hassen-Badi, Alger 16100, Algeria; Laboratoire EM.2.C.-Ecole Centrale-Paris, 92295, Chatenay-Malabry-Cedex, France
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/119/1/124/5889481/124_1.pdf
Reference10 articles.
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2. Ait-Ali, M. A., 1995, “Finite-Time Optimum Refrigeration Cycles,” J. Appl. Phys., Vol. 77(9).
3. Curzon F. L. , and AhlbornB., 1975, “Efficiency of a Carnot Engine at Maximum Power Output,” Am. J. Phys., Vol. 43, pp. 22–24.
4. De Lucia M. , BronconiR., and CarnevaleE., 1994, “Performance and Economic Enhancement of Cogeneration Gas Turbine Through Compressor Inlet Air Cooling,” ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER, Vol. 116, pp. 360–365.
5. Ibrahim O. M. , KleinS. A., and MitchellJ. W., 1991, “Optimum Heat Power Cycles for Specified Boundary Conditions,” ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER, Vol. 113, pp. 514–521.
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