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Experimental study of the shock wave due to a blunt leading edge in the hypersonic merged- flow regime

ROGER M. WINEBARGER

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Key concepts: Shock wave, Hypersonic speed, Mechanics, Hypersonic flow, Shock (circulatory), Leading edge, Flow (mathematics), Physics

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Experimental study of the shock wave due to a blunt leading edge in the hypersonic merged- flow regime — Research Paper | ScholarLens