Some aspects of modelling compressor behavior in Gas turbineperformance calculations

Journal of Turbomachinery

Volumn 123, Issue 2, 2001, Pages 372-378

  Riegler, C ^a   Bauer, M ^a   Kurzke, J ^a  

^a MTU AERO ENGINES GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; MAPS; ROTORS; TURBOFAN ENGINES;

TURBO COMPONENTS;

GAS TURBINES;

COMPRESSOR; GAS TURBINE; MATHEMATICAL ANALYSIS; MODELING;

EID: 0035299110     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1368123     Document Type: Article

References (9)

1. Gas turbine performance
2. How to get component maps for aircraft gas turbine performance calculations
3. Berücksichtigung des Einflusses des Isentropenexponenten auf die Kennfelder von Turbinen
4. Calculation of installation effects within performance computer programs
5. Engine-out performance characteristics
6. Turbinenkennfelderstellung für kleine Arbeiten und Drehzahlen
7. Smooth C 7.0: Preparing compressor maps for performance calculations
8. The stability of split flow fans