Mainstream aerodynamic effects due to wheelspace coolant injection in a high-pressure turbine stage: Part I - Aerodynamic measurements in the stationary frame

Journal of Turbomachinery

Volumn 123, Issue 4, 2001, Pages 687-696

  McLean, C ^a   Camci, C ^a   Glezer, B ^a  

^a Techkor Instrumentation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYER FLOW; COOLANTS; ROTORS;

COOLANT INJECTIONS;

TURBINES;

AERODYNAMICS; COOLANT; GAS TURBINE; MEASUREMENT METHOD;

EID: 0035483346     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1401026     Document Type: Article

References (22)

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3. Local heat transfer in turbine disk cavities: Part II-Rotor cooling with radial location injection of coolant
4. Über Llaminare und Turbulente Reibung
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7. Chamber dimensional effects on induced flow and frictional resistance of enclosed rotating disks
8. Jet cooling at the rim of a rotating disk
9. Local heat transfer from a rotating disk in an impinging round jet
10. Heat transfer measurements for rotating turbine disks
11. Chapter 33, gas turbine disk cooling flows
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13. Investigation of Three Dimensional Flow Field in a Turbine Including Rotor/Stator Interaction
14. Aerodynamic aspects of endwall film-cooling
15. Effects of Film Injection on Performance of a Cooled Turbine
16. ASME measurement uncertainty