1994•25th Plasmadynamics and Lasers ConferenceRequires access

On the design and testing of a Mach 6 nozzle for a shock reflect type hypersonic shock tunnel

Fan‐Ming Yu, M. Tyen, Y. Chen

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Key concepts: Mach number, Hypersonic speed, Shock (circulatory), Expansion tunnel, Nozzle, Aerospace engineering, Hypersonic wind tunnel, Aeronautics

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On the design and testing of a Mach 6 nozzle for a shock reflect type hypersonic shock tunnel — Research Paper | ScholarLens