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2021•Journal of the Korean Society of Propulsion EngineersOpen access

Effect of Nozzle Initial and Exit Wall Angles on Supersonic Flow Field in a Thrust Optimized Nozzle

Tae Jun Jeon, Tae Seon Park

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Key concepts: Nozzle, Thrust, Mechanics, Supersonic speed, Aerospace engineering, Choked flow, Flow (mathematics), Discharge coefficient

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