Some aspects of modelling compressor behavior in gas turbine performance calculations

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Riegler, Claus ^a   Bauer, Michael ^a   Kurzke, Joachim ^a  

^a MTU AERO ENGINES GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BYPASS RATIO; COMPRESSIBILITY OF GASES; COMPRESSORS; ENGINES; FIGHTER AIRCRAFT; GAS COMPRESSORS; MARINE ENGINES;

ENGINE COMPONENTS; GAS TURBINE PERFORMANCE; INDEPENDENT PARAMETERS; OPERATING CONDITION; PERFORMANCE CALCULATION; PERFORMANCE CHARACTERISTICS; PERFORMANCE MODELLING; SECOND ORDER EFFECT;

GAS TURBINES;

EID: 84955087092     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0574     Document Type: Conference Paper

References (9)

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3. Braig W. and Riegler C., 1994, Berucksichtigung des Einusses des Isentropenexponenten auf die Kennfelder von Turbinen. Forschung im Ingenieurwesen.
4. Kurzke J., 1992, Calculation of Installation Effects within Performance Computer Programs. In AGARD-LS-183, pages 71-719.
5. Kurzke J., 1996, How to get Component Maps for Aircraft Gas Turbine Performance Calculations. In International Gas Turbine and Aeroengine Congress and Exhibition, ASME 96-GT-164.
6. Kurzke J., 1999, Smooth C 7.0: Preparing Compressor Maps for Performance Calculations. User's Manual.
7. Therkorn D. and Braig W., 1994, Turbinenkennfelderstellung fur kleine Arbeiten und Drehzahlen. Zeitschrift fur Flugwissenschaften und Weltraumforschung, 18(2):140-144.
8. Tzannatos E. and Elder R. L., 1993, The Stability of Split Flow Fans. International Journal of Turbo and Jet Engines, 10:235-251.
9. Walsh P. P. and Fletcher P., 1998, Gas Turbine Performance. Blackwell Science.