Exergetic effects of some design parameters on the small turbojet engine for unmanned air vehicle applications

Energy

Volumn 46, Issue 1, 2012, Pages 51-61

  Turan, Onder ^a  

^a ANADOLU UNIVERSITY   (Turkey)

Author keywords

Auxiliary power unit; Exergy; Propulsion; Small turbojet; Unmanned air vehicle

Indexed keywords

AERODYNAMICS; MACH NUMBER; PROPULSION; TURBINES; UNMANNED AERIAL VEHICLES (UAV);

AUXILIARY POWER UNITS; COMPRESSOR PRESSURE RATIO; COMPUTER EXPERIMENT; DESIGN PARAMETERS; ENERGY AND EXERGY; EXERGY EFFICIENCIES; OPERATING PARAMETERS; SMALL TURBOJET; SMALL TURBOJET ENGINE; TURBINE INLET TEMPERATURE; UNMANNED AIR VEHICLE (UAVS);

EXERGY;

DATA SET; DESIGN; ENERGY EFFICIENCY; ENGINE; EXERGY; EXPERIMENTAL STUDY; PERFORMANCE ASSESSMENT; TURBINE; UNMANNED VEHICLE;

EID: 84867233470     PISSN: 03605442     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.energy.2012.03.030     Document Type: Article

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