引射火箭,rocket ejector英語短句,例句大全

引射火箭,rocket ejector
1)rocket ejector引射火箭
1.An investigation of the influence of secondary nozzles on the performance of rocket ejectors;二次噴管對引射火箭性能影響研究
2.Investigation on Performance and Influence Factors of Rocket Ejector Mode of RBCC;RBCC引射火箭模態性能與影響因素研究
3.Rocket ejector with strut characteristic was adopted.為了提高RBCC引射火箭模態的推力性能,探索熱力壅塞對引射模態推力的影響,開展了二次燃燒實驗研究。

英文短句/例句

1.Effects of incoming Mach number on secondary mass flow rate來流馬赫數對引射火箭引射量的影響研究
2.Investigation on Performance and Influence Factors of Rocket Ejector Mode of RBCC;RBCC引射火箭模態性能與影響因素研究
3.Influence of mixture ratio of primary flow on secondary combustion flame stability of ejector rocket motor一次燃氣混合比對引射火箭二次燃燒火焰穩定的影響
4.launch pad(火箭等的)發射臺
5.ballistic trajectory(火箭的)放射彈道
6.Combustion Flow Investigation in Ejecting Mode of RBCC;火箭基組合動力循環（RBCC）引射模態燃燒流動研究
7.Numerical simulation of ejector-ram-rocket propulsion system引射式火箭沖壓組合推進系統的數值仿真
8.Medium Artillery Rocket Launcher中型炮兵火箭發射器
9.ALSOR (Air Launched Sounding Rocket)空中發射的探測火箭
10.area within which rockets and missiles are fired（火箭和導彈的）發射場.
11.A rocket was fired at the moon.火箭發射到月球上。
12.nozzle junction assembly(火箭發射等) 導向器
13.non-propelling rocket laucher火箭發射裝置,非推進式
14.Quasi-One-Dimensional Theoretical Analysis of Ejector Mode of Rocket-Based Combined Cycle Engine火箭基組合循環發動機（RBCC）引射模態的準一維理論分析
15.The launching of a missile, rocket, or similar ballistic body.發射導彈、火箭或類似拋射物的發射
16.About half the launches trigger lightning from the clouds above, and the bolts usually strike the rocket launcher.約半數的發射任務會從上空的云層引發閃電，而雷電通常會擊中火箭發射臺。
17.The rocket lifted off from its launching pad.火箭從發射臺上發射出去。
18.To launch a rocket is to send it up from its launching pad.發射火箭就是從發射臺把它送上去。

相關短句/例句

rocket ejector mode火箭引射模態
1.An investigation of thermal choke in rocket ejector mode;RBCC火箭引射模態熱力壅塞研究
3)ejector rocket motor引射火箭發動機
1.Based on comprehensive analysis for combustion mode of ejector rocket,the numerical analysis of SMC+DAB hybrid combustion mode and direct connected experiments for the ejector rocket motor with fixed structure were carryied out by means of the essential principle of dual-combustor ramjet.在綜合分析引射火箭燃燒組織模式的基礎上,針對固定結構的引射火箭發動機,借助雙燃燒室沖壓發動機的原理,開展了SMC+DAB混合燃燒組織模式的數值分析和發動機直連實驗研究,詳細分析了富燃一次燃氣對二次燃燒火焰穩定的作用及其對發動機性能的影響。
4)rocket triggered lightning火箭引雷
1.The paper introduces the rocket triggered lightning test to conventional lightning rod and a novel lightning protection device called semiconductor lightning eliminator(SLE),which has the ability to limit lightning current.介紹了對普通避雷針和半導體消雷器進行的火箭引雷試驗,列出了全部試驗結果,包括用普通照相機的B門進行靜態拍攝所得的典型照片以及用示波器記錄的雷電流波形。
5)rocket engine火箭引擎
6)Submarine rocket潛射火箭