Incidence Effects on Wake-Induced Transition on an Axial Compressor Blade
Author:
Affiliation:
1. Ohio Aerospace Institute/General Electric Aircraft Engines, Cincinnati, Ohio 45215
2. University of Tasmania, Hobart, Tasmania 7001, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5603
Reference30 articles.
1. Local Heat Transfer Measurements on a Gas Turbine Blade
2. Boundary-Layer Transition and Separation Near the Leading Edge of a High-Speed Turbine Blade
3. Boundary Layer Development on Turbine Airfoil Suction Surfaces
4. Simulation of wake passing in a stationary turbine rotor cascade
5. Measurement and Modeling of the Gas Turbine Blade Transition Process as Disturbed by Wakes
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