Blade heat transfer measurements and predictions in a transonic turbine cascade

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1999, Pages

  Giel, P W ^a   Van Fossen, G J ^b   Boyle, R J ^b   Thurman, D R ^c   Civinslcas, K C ^c  

^a Dynacs Engineering Company Inc   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c U S ARMY RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC TEMPERATURE; BENCHMARKING; BOUNDARY LAYERS; CALIBRATION; COMPUTATIONAL FLUID DYNAMICS; FORECASTING; GAS TURBINES; HEAT RESISTANCE; INLET FLOW; LIQUID CRYSTALS; REYNOLDS NUMBER; TURBINE COMPONENTS; TURBOMACHINE BLADES; TURBULENCE;

HEAT TRANSFER MEASUREMENTS; INLET BOUNDARY LAYER; LAMINAR TO TURBULENT TRANSITIONS; STEADY STATE TECHNIQUES; SURFACE HEAT TRANSFER; THREE DIMENSIONAL FLOW FIELD; TRANSONIC TURBINE CASCADE; TURBULENCE INTENSITY;

HEAT TRANSFER;

EID: 84928494193     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-125     Document Type: Conference Paper

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