Parametric comparative study of Rocket Nozzle Convective Heat Transfer Coefficient Application of Combustion gas characteristic and Method of Analysis (해석방법 및 연소가스특성 적용에 따른 로켓 노즐 대류열전달계수의 매개변수적 비교 고찰)
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- Proceedings of the Korean Society of Propulsion Engineers Conference
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- 2017.05a
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- pp.651-663
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- 2017