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2015•Unpublished venueRequires access

Aerodynamic Control Effect of Surface DC Plasma Discharge at Mach-7 Hypersonic Flow

Yasumasa Watanabe, Kojiro Suzuki

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Key concepts: Aerodynamics, Mach number, Hypersonic speed, Hypersonic flow, Aerospace engineering, Aerodynamic heating, Flow control (data), Plasma

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Aerodynamic Control Effect of Surface DC Plasma Discharge at Mach-7 Hypersonic Flow — Research Paper | ScholarLens