1998•8th AIAA International Space Planes and Hypersonic Systems and Technologies ConferenceRequires access

Experimental investigation of shock wave/boundary layer interactions over an artificially heated model in hypersonic flow

Fabrizio Scortecci, Fabrizio Paganucci, Luca d’Agostino

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Key concepts: Hypersonic flow, Boundary layer, Hypersonic speed, Shock wave, Mechanics, Flow (mathematics), Aerospace engineering, Shock (circulatory)

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Experimental investigation of shock wave/boundary layer interactions over an artificially heated model in hypersonic flow — Research Paper | ScholarLens