Influence of compressor deterioration on engine dynamic behavior and transient stall-margin

Journal of Turbomachinery

Volumn 122, Issue 3, 2000, Pages 477-484

  Spakovszky, Z S ^a   Gertz, J B ^a   Sharma, O P ^a   Paduano, J D ^a   Epstein, A H ^a   Greitzer, E M ^a  

^a Massachusetts Institute of Technology Cambridge   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; COMPRESSORS; COMPUTER SIMULATION; DETERIORATION; MATHEMATICAL MODELS; PRESSURE MEASUREMENT; ROTORS; STATE SPACE METHODS;

COMPRESSOR DETERIORATION; TRANSIENT STALL MARGIN;

AIRCRAFT ENGINES;

COMPRESSOR; DYNAMIC BEHAVIOR; STALL;

EID: 0034233179     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1303817     Document Type: Conference Paper

References (10)

1. Compressor surge and stall propagation
2. A theory of rotating stall of multistage axial compressors: Part I-small disturbances
3. A theory of post-stall transients in axial compressors: Part I-development of the equations
4. Modelling high speed multistage compressor stability
5. Modeling for control of rotating stall in high speed multi-stage axial compressors
6. Pre-stall behavior of several high-speed compressors
7. Implications of stability modeling for high-speed axial compressor design
8. Active stabilization of rotating stall and surge in a transonic single stage axial compressor
9. Simulation of engine clearances effects on compressor dynamic behaviour during acceleration transients
10. Analysis of instability inception in high-speed multistage axial-flow compressors