飛機外掛物 的英文怎麼說

中文拼音 [fēiwàiguà]
飛機外掛物 英文
aircraft stores
  • : Ⅰ動詞1 (鳥、蟲等在空中活動) fly; flit 2 (利用動力機械在空中行動) fly 3 (在空中飄浮遊動) fly...
  • : machineengine
  • : Ⅰ名詞1 (外面) outside; external side 2 (外國) foreign country 3 (以外) besides; beyond; in ...
  • : Ⅰ動詞1 (使物體附著于某處) hang; put up; suspend 2 (中斷電話) ring off 3 [方言] (接通電話; 打...
  • : 名詞1 (東西) thing; matter; object 2 (指自己以外的人或與己相對的環境) other people; the outsi...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  1. The chimera embedding technique is presented for the external store separation configuration. it divides the whole region into many subdomains. euler equations are used for every subregion with the finite volume method

    本文採用嵌套網格技術,將投放的模型分成多個計運算元域,對投放的復雜形進行了分區迭代求解。
  2. During helicopter slung - load flight, the main flight quality modes include : phugoid, dutch roll, longitude and latitude slung - load oscillation. according to the ads - 33e - prf specifications, the flight stability qualities had been evaluated

    直升行過程中,體現行品質的運動模態主要為荷蘭滾模態、縱向浮沉振蕩模態,以及吊橫向、縱向振蕩模態。
  3. The main factors which affected the flight stability quality included : forward flight speed, slung - load and helicopter mass ration, slung - load aerodynamic forces and cable length, etc. through adjusting the above structure and performance parameters, rational flight parameters can be decided, which can ensure the safe helicopter mission operations of the slung - load flight

    影響行品質穩定性要求的主要因素為:直升行速度、吊/直升質量比、吊氣動特性、吊鋼索長度等。通過對上述結構參數、性能參數的調節,可確定合理、經濟的行參數,保證安全、高效的完成直升行運輸任務。
  4. During its storage, transportation, maintenance and service, the solid rocket motor ( srm ) may encounter many incidents such as being dropped onto the ground while being hoisted up, crashing when vehicle turns over during transportation, being struck heavily in takeoff or landing accident while being carried by airplane, impacting with launch platform or buildings when there is abnormality during launch of multiple - stage rocket. impact of great intensity takes place in such accidents, which will lead to srm ignition or explosion

    固體火箭發動在貯存、運輸、維護及使用過程中可能遇到各種意械撞擊激勵,例如:吊裝過程中跌落,運輸過程中因交通事故發生翻覆碰撞,載固體導彈時因載發生起降事故導致高速沖撞,多級火箭發射初期因發射異常與發射架或地面建築發生碰撞等,固體火箭發動將受到劇烈械撞擊載荷作用,導致其著火燃燒甚至爆炸。
  5. The prediction of the separation trajectories of the external stores carried out on aircraft is an important task in the aerodynamic design area

    投放的分離軌跡預測在氣動設計領域是一個很重要的課題。
  6. The investigation of the distribution of aerodynamic forces on the external stores and their neighboring aircraft surfaces during the transient process of the separation of the external store from an aircraft is an urgent need because aerodynamic interactions can cause the released store to impact upon, and possibly damage, the aircraft

    從載上發射導彈、投擲炸彈或拋棄副油箱時,處于載復雜干擾流場中。此時往往出現不正常分離,有時會導致與載發生碰撞,嚴重危及載行人員安全的重大事故。
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