Three imensional flow field measurements in a transonic turbine cascade

ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996

Volumn 1, Issue , 1996, Pages

  Giel, P W ^a   Thurman, D R ^b   Lopez, I ^b   Boyle, R J ^c   Van Fossen, G J ^c   Jett, T A ^c   Camperchioli, W P ^c   La, H ^c  

^a NYMA Inc   (United States)

^b U S ARMY RESEARCH LABORATORY   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BENCHMARKING; BOUNDARY LAYERS; FLOW FIELDS; FLOW OF FLUIDS; GAS TURBINES; INLET FLOW; MACH NUMBER; NASA; PROBES; REYNOLDS NUMBER; TURBINE COMPONENTS; TURBOMACHINE BLADES;

FLOW FIELD MEASUREMENT; MEASUREMENT PLANES; MEASUREMENTS OF; MODEL VERIFICATION; STATIC PRESSURE; THREE DIMENSIONAL FLOW FIELD; TRANSONIC TURBINE; TRANSONIC TURBINE CASCADE;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84923923893     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-113     Document Type: Conference Paper

References (17)

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