Investigation of unsteady flow through a transonic turbine stage. II- Data/prediction comparison for time-averaged and phase-resolved pressure data-Reference-Cited by-同舟云学术

Investigation of unsteady flow through a transonic turbine stage. II- Data/prediction comparison for time-averaged and phase-resolved pressure data

Published:1990-07-16 Issue: Volume: Page:
ISSN:
Container-title:26th Joint Propulsion Conference
language:
Short-container-title:

Author:

DUNN M.¹,BENNETT W.²,DELANEY R.²,RAO K.²

Affiliation:

1. Calspan Corp., Buffalo, NY

2. General Motors Corp., Allison Gas Turbine Div., Indianapolis, IN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2409

Reference25 articles.

1. Blair, M.F., Dring, R.P., and Joselyn, H.D., 1988, "The Effects of Turbulence and RotorIStator Interaction on the Heat Transfer of a Large Rotating Turbine Model, Part I and 11," ASME papers 88-GT-5 and 88-GT-6.

2. An Experimental Investigation of Film Cooling on a Turbine Rotor Blade

3. Measurement of Turbine Rotor Blade Flows

4. Turbine Rotor-Stator Interaction

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