AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.89, no.5, pp.719-724, 2017 (SCI-Expanded)
Article / Article
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
Science Citation Index Expanded (SCI-EXPANDED), Scopus
Exergy, Gas turbine, Propulsion, Combustor, Turbojet, BYPASS TURBOFAN ENGINE, TURBINE POWER-PLANTS, TURBOPROP ENGINE, GENERATION, EFFICIENCY, ALGORITHM, ENERGY, AID
Anadolu University Affiliated:
Purpose - The purpose of this study is to perform an exergy analysis of a turbojet engine combustor at different cycle parameters. Design/methodology/approach - Base cycle parameters have been defined for the engine, and then differentiation of the combustor exergy efficiencies and destruction rates have been evaluated by changing overall pressure ratio, combustor exit temperature and combustor pressure ratio.