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Flow Control of Swept Shock-Wave/Boundary-Layer Interaction Using Plasma Actuators
Author(s) -
Akshay S. Deshpande,
Jonathan Poggie
Publication year - 2018
Publication title -
journal of spacecraft and rockets
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.758
H-Index - 79
eISSN - 1533-6794
pISSN - 0022-4650
DOI - 10.2514/1.a34114
Subject(s) - plasma actuator , mechanics , boundary layer , flow separation , mach number , reynolds number , materials science , shock wave , oblique shock , vortex , boundary layer thickness , physics , plasma , quantum mechanics , dielectric barrier discharge , turbulence

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