Demonstration of Separation Control Using Dielectric Barrier Discharge Plasma Actuators
Author:
Affiliation:
1. NASA John H. Glenn Research Center, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056976
Reference55 articles.
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3. HourmouziadisJ. “Aerodynamic Design of Low Pressure Turbines,” AGARD Lecture Series 167, Neuilly-Sur-Seine, France, 1989.
4. SharmaO. P.NiR. H.TanrikutS. “Unsteady Flow in Turbines,” AGARD Lecture Series LS-195, Neuilly-Sur-Seine, France, 1994, Paper 5.
5. Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions—Part 1: Mean Flow and Turbulence Statistics
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