Separation Control on a Low-Pressure Turbine Blade using Microjets
Author:
Affiliation:
1. Department of Mechanical Engineering, Florida A&M University and Florida State University, Tallahassee, Florida 32310
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/10.2514/1.B34413
Reference32 articles.
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3. On the Impact of Blade Count Reduction on Aerodynamic Performance and Loss Generation in a Three-Stage LP Turbine
4. Experimental Demonstration of Active Flow Control to Reduce Unsteady Stator-Rotor Interaction
5. Control of circular cylinder flow by the use of dimples
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