Control of Separation in Turbine Boundary Layers
Author:
Affiliation:
1. Air Force Research Laboratory
2. Brigham Young University
3. Institute of Hydromechanics NASU
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2201
Reference58 articles.
1. Helton,D.,privatecommunication,1997.
2. Qiu, S. and Simon, T. "An Experimental Investigation of Transition as Applied to Low Pressure Turbine Suction Surface Flows",ASME 97-GT-455, 1997.
3. Experimental Investigation of Boundary Layer Behavior in a Simulated Low Pressure Turbine
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