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Investigation on Oblique Shock Wave Control by Surface Arc Discharge in a Mach 2.2 Supersonic Wind Tunnel

Yinghong Li, Jian Wang

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Abstract

Mach 2.2 Supersonic Wind Tunnel, Wind Tunnels and Experimental Fluid Dynamics Research, Prof.

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Mach 2.2 Supersonic Wind Tunnel, Wind Tunnels and Experimental Fluid Dynamics Research, Prof.

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OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Mach 2.2 Supersonic Wind Tunnel, Wind Tunnels and Experimental Fluid Dynamics Research, Prof.

Key concepts: Shock wave, Oblique shock, Supersonic speed, Mach number, Sonic boom, Bow shock (aerodynamics), Mechanics, Shock diamond

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