Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Van Zante, Dale E ^a   Strazisar, Anthony J ^a   Wood, Jerry R ^a   Hathaway, Michael D ^b   Okiishi, Theodore H ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b US Army Vehicle Technology Directorate   (United States)

^c IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; DOPPLER EFFECT; GAS TURBINES; LASER DOPPLER VELOCIMETERS; LEAKAGE (FLUID); NASA; NAVIER STOKES EQUATIONS; NUMERICAL MODELS; SUPERSONIC AIRCRAFT; TRANSONIC FLOW; TURBULENCE MODELS;

HIGH SPEED MACHINE; LASER DOPPLER VELOCIMETER (LDV); LOCAL EQUILIBRIUM; SIMULATED RESULTS; SIMULATION ACCURACY; STAGE PERFORMANCE; TIP CLEARANCE FLOW; TRANSONIC COMPRESSOR ROTOR;

SHEAR FLOW;

EID: 84890131308     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-390     Document Type: Conference Paper

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