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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.26 no.2, 2022년, pp.1 - 11
노태원 (Department of Aerospace Engineering, Inha University) , 노태성 (Department of Aerospace Engineering, Inha University) , 이형진 (Department of Aerospace Engineering, Inha University) , 이현섭 (Rocket Propulsion, Mechanical R&D, LIG Nex1) , 유필훈 (Rocket Propulsion, Mechanical R&D, LIG Nex1)
The heat transfer coefficient on the wall, which is used as a boundary condition in the thermal analysis of general contract-divergent supersonic nozzles, affects the thermal analysis accuracy of the entire nozzle. Accordingly, many methods of deriving a heat transfer coefficient have been proposed....
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