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contributor authorW. H. Heiser
contributor authorT. Huxley
contributor authorJ. W. Bucey
date accessioned2017-05-09T00:43:26Z
date available2017-05-09T00:43:26Z
date copyrightNovember, 2011
date issued2011
identifier issn1528-8919
identifier otherJETPEZ-27176#111702_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145898
description abstractThis paper presents the results of a fundamental, comprehensive, and rigorous analytical and computational examination of the performance of the Brayton propulsion and power cycle employing real air as the working fluid. This approach capitalizes on the benefits inherent in closed cycle thermodynamic reasoning and the behavior of the thermally perfect gas to facilitate analysis. The analysis uses a high fidelity correlation to represent the specific heat at constant pressure of air as a function of temperature and the polytropic efficiency to evaluate the overall efficiency of the adiabatic compression and expansion processes. The analytical results are algebraic, transparent, and easily manipulated, and the computational results present a useful guidance for designers and users. The operating range of design parameters considered covers any current and foreseeable application. The results include some important comparisons with more simplified conventional analyses.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Brayton Cycle Using Real Air and Polytropic Component Efficiencies
typeJournal Paper
journal volume133
journal issue11
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4003671
journal fristpage111702
identifier eissn0742-4795
keywordsPressure
keywordsSpecific heat
keywordsHeat
keywordsTemperature
keywordsBrayton cycle
keywordsCompression
keywordsCycles AND Equations
treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 011
contenttypeFulltext


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