Exergetic Destruction Effects of Operating Conditions on the Turbojet Engine Components

Abstract:

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The minimization of exergy destruction brings the design as closely as permissible to the theoretical limit. This study presents exergy destruction analysis of a turbojet engine for different flight Mach number and altitudes. Turbojet engine being considered consists of an inlet, a centrifugal compressor, reverse flow combustion chamber, axial-flow turbine and exhaust nozzle. The flight Mach number and altitude are examined on the exergetic destructions of compressor, combustion chamber, turbine and exhaust nozzle. The results of component-based destruction analysis are given as three dimensional exergetic-destruction response surface plots related to altitude and flight Mach number.

Info:

Periodical:

Edited by:

Wu Fan

Pages:

2390-2394

DOI:

10.4028/www.scientific.net/AMM.110-116.2390

Citation:

T. H. Karakoc and O. Turan, "Exergetic Destruction Effects of Operating Conditions on the Turbojet Engine Components", Applied Mechanics and Materials, Vols. 110-116, pp. 2390-2394, 2012

Online since:

October 2011

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Price:

$35.00

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