Compressor stability enhancement using discrete tip injection

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Suder, Kenneth L ^a   Hathaway, Michael D ^b   Thorp, Scott A ^a   Strazisar, Anthony J ^a   Bright, Michelle B ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

^b US Army Vehicle Technology Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL FLOW TURBOMACHINERY; COMPRESSORS; NAVIER STOKES EQUATIONS; STABILITY; SUPERSONIC AIRCRAFT; UNLOADING;

ANNULAR INJECTION; CASING TREATMENT; COMPRESSOR STABILITY; FLOW COEFFICIENTS; HIGH-SPEED AXIAL COMPRESSORS; INJECTION VELOCITY; STABILITY ENHANCEMENT; TRANSONIC AXIAL COMPRESSORS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84856426403     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0650     Document Type: Conference Paper

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