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한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.26 no.2, 2022년, pp.72 - 78
한명재 (Precision Guided Munition R&D Group, LIG Nex1) , 설진운 (Precision Guided Munition R&D Group, LIG Nex1) , 정승호 (Precision Guided Munition R&D Group, LIG Nex1) , 차민경 (Precision Guided Munition R&D Group, LIG Nex1) , 장호연 (Aerospace R&D Center, Hanwha Aerospace) , 김중회 (Aerospace Tech. -3rd, Agency for Defense Development)
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A vacuum brazed cooling passage for an aircraft engine controller was designed. In order to predict the total pressure loss, which is the main design factor of the cooling passage, theoretical and numerical methods for the major loss and the minor loss considering the overall shape of the cooling pa...
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