Stall inception in a 5-stage HP-compressor with increased load due to inlet distortion

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Jahnen, Werner ^a   Peters, Thomas ^b   Fottner, Leonhard ^b  

^a Sulzer Ltd   (Switzerland)

^b BUNDESWEHR UNIVERSITY MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMPRESSORS; DAMPING; GAS TURBINES; STABILITY;

COMPRESSOR MODELING; DIFFERENT SPEED; DIFFUSION FACTOR; HOT WIRE MEASUREMENTS; INLET DISTORTION; LINEAR STABILITY PROPERTIES; MEASUREMENTS OF; STALL INCEPTION;

INLET FLOW;

EID: 84928545234     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-440     Document Type: Conference Paper

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