Endwall heat transfer measurements in a transonic turbine cascade

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

Volumn 4, Issue , 1996, Pages

  Giel, P W ^a   Thurman, R ^b   Van Fossen, G J ^c   Hippensteele, S A ^c   Boyle, R J ^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; COMPUTATIONAL FLUID DYNAMICS; FLOW FIELDS; GAS TURBINES; HEAT TRANSFER; INLET FLOW; LIQUID CRYSTALS; MACH NUMBER; NASA; REYNOLDS NUMBER; TURBOMACHINE BLADES;

FREESTREAM TURBULENCE INTENSITY; HEAT TRANSFER DATA; HEAT TRANSFER MEASUREMENTS; INLET CONDITIONS; LIQUID-CRYSTAL TECHNIQUE; MODEL VERIFICATION; TRANSONIC TURBINE; TRANSONIC TURBINE CASCADE;

TURBINE COMPONENTS;

EID: 84923870778     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-180     Document Type: Conference Paper

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