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Investigations in Supersonic Flow I. Design of a Supersonic Wind Tunnel II. Curved Shocks in Mach Reflection

Howard Reiss

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Key concepts: Supersonic wind tunnel, Supersonic speed, Choked flow, Mach number, Mach reflection, Wind tunnel, Reflection (computer programming), Physics

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Investigations in Supersonic Flow I. Design of a Supersonic Wind Tunnel II. Curved Shocks in Mach Reflection — Research Paper | ScholarLens