Effects of Finite-Rate Chemistry and Film Cooling on Linear Combustion-Stability Limit in Liquid Rocket Engine (액체 로켓엔진에서 선형 연소 안정한계에 미치는 유한화학반응 및 막냉각 효과)
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- Journal of the Korean Society for Aeronautical & Space Sciences
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- v.34 no.2
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- pp.75-81
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- 2006