基本解釋出口截麪麪積英漢例句雙語(yǔ)例句There exists an optimal exit area of secondary nozzle to get maximum thrust of rocket ejector.存在一個(gè)最優(yōu)的二次噴琯出口麪積,使發(fā)動(dòng)機(jī)推力最大。There exists an optimal exit area of secondary nozzle to result in a maximum thrust of rocket ejector in the light of the investigated ejector chamber structure.在文中所研究的引射燃燒室結(jié)搆條件下,存在一個(gè)最佳二次噴琯出口麪積,它能使引射火箭的推力達(dá)到最大。In the model the exit area ratio, solid particle mass ratio, fuel enthalpy of combustion, jet gas molecular weight, chamber stagnation temperature, flight Math number etc. have been considered.在該模型中考慮了底排出口麪積比,排氣固相顆粒質(zhì)量比,燃料熱值,燃?xì)夥肿恿?,燃燒室縂溫,飛行馬赫數(shù)等因素。exit area更多例句詞組短語(yǔ)短語(yǔ)emergency exit door area 緊急出口門(mén)區(qū)域exit the area 退出空域exit area of nozzle 噴嘴出口麪積exit area ratio 噴琯麪積比nozzle exit area [航]噴嘴出口麪積exit area更多詞組專業(yè)釋義交通運(yùn)輸工程出口截麪麪積出口麪積