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한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.27 no.1, 2023년, pp.27 - 36
안현종 (Department of Mechanical Engineering, Graduate School, Pukyong National University) , 강윤형 (Department of Mechanical Engineering, Graduate School, Pukyong National University) , 김정수 (School of Mechanical Engineering, Pukyong National University)
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To understand the atomization performance in gas-liquid swirl-coaxial injector applied to a small rocket engine, a cold-flow test was performed by varying the design parameters and supply condition of propellants. As the swirl-chamber diameter and the angle of the convergent section, which are desig...
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