Christoph Hollenstein, Peter Ott, Pénélope Leyland, Philip Peschke, Sami Goekce
Experiments were conducted in order to investigate the ability of nanosecond pulsed dielectric barrier discharge (ns-DBD) actuators to control flow on airfoils in subsonic and transonic flow (up to Ma1 = 0.75, Re = 1.35 • 10^6). A NACA 0015 profile equippe ...
The American Institute of Aeronautics and Astronautics2013