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

Journal of the Korean Society of Propulsion Engineers Pub Date : 2021-06-30 DOI:10.6108/kspe.2021.25.3.001
T. Jeon, T. Park
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Journal of the Korean Society of Propulsion Engineers
Journal of the Korean Society of Propulsion Engineers
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