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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.25 no.4, 2021년, pp.53 - 58
송주연 (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) , 최명환 (Department of Smart Drone Convergence, Korea Aerospace University) , 안정우 (Department of Smart Drone Convergence, Korea Aerospace University) , 구자예 (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
Based on surrogate model, a hydrocarbon mixture was analyzed by visualizing the impinging break up mechanism in subcritical and supercritical conditions. Decane and methylcyclohexane with different critical pressures and temperatures were selected as experimental fluids. The impinging injector was i...
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