Heat-transfer measurements and predictions for the vane and blade of a rotating high-pressure turbine stage

Journal of Turbomachinery

Volumn 126, Issue 1, 2004, Pages 101-109

  Haldeman, Charles W ^a   Dunn, Michael G ^a  

^a OHIO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; DATA REDUCTION; HEAT TRANSFER; THERMAL BARRIER COATINGS; TURBINES; TURBOMACHINE BLADES; VANE PUMPS;

ENDWALLS; OFF-MIDSPAN LOCATIONS; ROTATING HIGH-PRESSURE TURBINES; THERMAL-BARRIER-COATED VANES;

AERODYNAMICS;

HEAT TRANSFER; MEASUREMENT METHOD; PREDICTION; PRESSURE; TURBINE;

EID: 1942506584     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1626132     Document Type: Article

References (31)

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4. Rivir, R. B., Elrod, W. C., and Dunn, M. G., 1985, "Two Spot Laser Velocimeter Measurements of Velocity and Turbulence Intensity in Shock Tube Driven Turbine Flows," AGARD Heat Transfer and Cooling in Gas Turbines, Conf. Proc. No. 390, pp. 33-1 to 33-12, Bergen, Norway.
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