火箭推进
火箭推進
화전추진
JOURNAL OF ROCKET PROPULSION
2012年
2期
56-62
,共7页
孔龙飞%夏智勋%胡建新%王德全
孔龍飛%夏智勛%鬍建新%王德全
공룡비%하지훈%호건신%왕덕전
粉末燃料冲压发动机%燃料供应%扰流锥体%两相流
粉末燃料遲壓髮動機%燃料供應%擾流錐體%兩相流
분말연료충압발동궤%연료공응%우류추체%량상류
powdered fuel ramjet%fuel feeding%fluid disturbing cone%two-phase flow
在粉末燃料冲压发动机的粉末燃料供应装置流化喷管处增设扰流锥体,并针对扰流锥体不同结构外形和位置对流场中离散相颗粒浓度的影响进行了计算分析,总结出了冷态下扰流锥体对外流场颗粒浓度分布的影响规律。
在粉末燃料遲壓髮動機的粉末燃料供應裝置流化噴管處增設擾流錐體,併針對擾流錐體不同結構外形和位置對流場中離散相顆粒濃度的影響進行瞭計算分析,總結齣瞭冷態下擾流錐體對外流場顆粒濃度分佈的影響規律。
재분말연료충압발동궤적분말연료공응장치류화분관처증설우류추체,병침대우류추체불동결구외형화위치대류장중리산상과립농도적영향진행료계산분석,총결출료랭태하우류추체대외류장과립농도분포적영향규률。
A fluid disturbing cone was set behind the nozzle of the powdered fuel feeding system in powdered fuel ramjet.A numerical simulation method was adopted to analyze the effects of its structures and position on the discrete phase particle concentration in cold flow field.The law that the fluid disturbing cone in cold state affects the particle concentration distribution in external flow field is presented.