PERFORMANCE PARAMETERS FOR GAS GENERATOR COMPARISON
Methods for comparing gas turbine engines where the thermodynamic cycle begins and ends in the atmosphere are well defined and documented. No such comparison technique (s) exists for the gas generator or core portion of the engine. The term gas generator or core refers to the high pressure compressor and turbine, and the combustor. The thesis formulates gas generator performance parameters, develops methods of testing and data reduction necessary to obtain these parameters, establishes criteria for comparing two gas generators, and develops an analytical model to test the validity of the comparison method.
Naval Postgraduate School1 University Circle
Monterey, CA United States 93943
- Burns, R J
- Publication Date: 1972-5
- Pagination: 86 p.
- TRT Terms: Computer aided design; Gas turbines; Mathematical models; Performance; Propulsion
- Old TRIS Terms: Propulsion machinery
- Subject Areas: Marine Transportation; Vehicles and Equipment;
- Accession Number: 00035594
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: MA Thesis
- Files: TRIS
- Created Date: Oct 27 1973 12:00AM