Detailed boundary layer measurements on a turbine stator vane at elevated freestream turbulence levels

Journal of Turbomachinery

Volumn 124, Issue 1, 2002, Pages 107-118

  Radomsky, R W ^a   Thole, K A ^a  

^a Virginia Polytechnic Institute and State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; HEAT TRANSFER; TURBULENCE; VELOCITY MEASUREMENT;

FREESTREAM TURBULENCE;

GAS TURBINES;

AEROFOIL; BOUNDARY LAYER; FLOW MEASUREMENT; GAS TURBINE; HEAT TRANSFER ENHANCEMENT; STATOR; TURBULENCE; VANE;

EID: 0036184580     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1424891     Document Type: Article

References (25)

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6. Detailed velocity and turbulence measurements of the profile boundary layer in a large scale turbine cascade
7. Boundary layer measurements on the pressure and suction sides of a turbine inlet guide vane
8. Flow characteristics of transitional boundary layers on an airfoil in wakes
9. High freestream turbulence effects on turbulent boundary layers
10. High freestream turbulence effects in the endwall leading edge region
11. Heat transfer and flowfield measurements in the leading edge region of a stator vane endwall
12. Flowfield measurements in the endwall region of a stator vane
13. Measurements and predictions of a highly turbulent flowfield in a turbine vane passage
14. Describing the uncertainties in experimental results
15. Approximate calculation of the laminar boundary layer
16. The effects of adverse pressure gradients on momentum and thermal structures in transitional boundary layers: Part 1-mean quantities
17. On the approximate integration of the differential equations of laminar shear layers
18. The effects of adverse pressure gradients on momentum and thermal structures in transitional boundary layers: Part 2-fluctuation quantities