An investigation of physics and control of flow passing a NACA0015 in fully reversed condition
Ohio State University Columbus United States
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Flow control experiments were performed on a NACA 0015 airfoil in fully-reversed condition, which is anticipated to occur on the retreating blade side of advancedhelicopters such as slowed-rotor compound rotorcraft. Control was achieved using nanosecond dielectric barrier discharge NS-DBD plasma actuators.
- Fluid Mechanics