Closed-Loop Control of Dynamic Oblique Shock with Arc Plasma
Fan Liu,
Bo Wang,
Hongchao Huang
et al.
Abstract:The fluctuations caused by the dynamic shock wave and its interaction with the boundary layer bring formidable challenges for aerodynamic design and stable control of supersonic aircraft. The mechanism of closed-loop control for dynamic oblique shock stabilizing with arc plasma is numerically studied. Two types of dynamic oblique shocks are formed in supersonic airflow by a compression ramp rotation and incoming Mach number variation, respectively. A closed-loop controller is established to connect the arc pla… Show more
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