箭反彈 的英文怎麼說

中文拼音 [jiànfǎndàn]
箭反彈 英文
arrow rebounding
  • : 名詞(古代兵器) arrow
  • : Ⅰ名詞1 (方向相背) reverse side 2 (造反) rebellion 3 (指反革命、反動派) counterrevolutionari...
  • : 彈名詞1. (彈子; 小球形的東西) ball; pellet 2. (內裝爆炸物, 具有破壞和殺傷能力的東西) bullet; bomb
  1. Figure 7. thrombus in a vein ( arrows ), identified by the absence of elastic fibers ( resorcin ? fuchsin elastic tissue stain, ? 125 ). in contrast, a nearby artery contains internal elastic fibers ( arrowhead )

    圖7 .血管缺乏性纖維,證明為靜脈,並見靜脈血栓(頭) 。相,附近的動脈存在性纖維。
  2. Iraqi insurgent leader claims group producing own rockets

    伊拉克叛領導稱已開始自行製造火
  3. Abstract : solid propellant rocket motors are preferred for most ballistic missiles because they need simple maintenance and can be launched quickly. but the conventional thrust termination devices limit the depletion of every stage ' s grain and increase some extra - weight. an improved method for designing a multi - stage solid rocket based depleted shutdown was provided. in order to solve the problem of lack of thrust termination devices, a device to adjust the burnout angle will match the final burnout velocity and satisfy the desired range. the method can also limit the detection from anti - ballistic missile system

    文摘:由於維護簡單和發射快速,道導多用固體火發動機,但繁雜的推力終止裝置使各級裝藥不能耗盡並讓結構增重.提出了一種對基於耗盡關機多級固體火概念設計的改進方法,此方法滿足導系統主要的戰技要求.為解決無推力終止裝置的末速不準問題,可在末級發動機採用姿態調整裝置,對射角進行調整,配合末速以滿足射程要求.本方法還可抑制敵方導探測
  4. The weapons are tow missile, two 7. 62mm or one 12. 7mm fn gun pod, one 70mm 7 rounds or 12 rounds pod

    武器包括「陶」式坦克導,裝兩挺7 . 62毫米或一挺12 . 7毫米機槍的fn武器吊艙和70毫米火的7管或12管發射巢。
  5. Collaborative optimization method is studied in depth, the causes leading to computational difficulty of this method are discussed by optimization theory and computation examples, and improve method which may solve this problem is presented. based on the comparison of several optimization methods and the characteristics of modern rocket - ramjet, step optimization pattern - a new integrated design mode is presented and is used to realize integrated design of rocket - ramjet. inner and outer fiowfield of a certain integral rocket - ramjet missile is simulated numerically using n - s equation

    ( 2 )系統地研究了導總體優化設計方法,探討了多學科設計優化的原理、框架結構、具體表述形式,深入研究了協作優化方法的原理,從優化原理和算例兩方面討論了造成協作優化方法計算困難的原因,提出了可能克服這種計算困難的改進途徑;在比較幾種優化方法的基礎上,針對新一代沖壓式導的特點,提出了一體化設計的模式? ?分步優化模式,進行了整體式火沖壓發動機艦導總體參數的一體化設計。
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