空戰教練機 的英文怎麼說

中文拼音 [kōngzhànjiāoliàn]
空戰教練機 英文
togun
  • : 空Ⅰ形容詞(不包含什麼; 裏面沒有東西或沒有內容; 不切實際的) empty; hollow; void Ⅱ名詞1 (天空) s...
  • : 教動詞(把知識或技能傳給人) teach; instruct
  • : Ⅰ名詞1 (白絹) white silk 2 (姓氏) a surname Ⅱ動詞1 (加工處理生絲) treat soften and whiten s...
  • : machineengine
  • 空戰 : air battle; aerial combat; air action; aerial engagement; air to air combat; air to air warfare空...
  • 教練機 : aircraft trainer
  • 教練 : 1. (訓練) train; drill; coach; practise 2. (教練員) coach; trainer; instructor
  1. In the french air force, mirage 2000 fighters in operation are : mirage 2000c / b single seater and two seater for air defence ; mirage 2000n, two seater, designed for all weather nuclear penetration at low altitude and very high speed ; and mirage 2000d, which is an upgraded version of the mirage 2000n, for automated bombing using conventional and laser guided munitions ; e type for multi purpose exporting version ; r for single seat day / night eaporting version

    在法國軍內,現役的幻影2000為幻影2000c型單座、 b型雙座、幻影2000n雙座全天候低高速核攻擊以及其改進型d型常規精確制導武器攻擊、幻影2000e多任務出口型、幻影2000r單座晝夜偵察出口型。
  2. The ten - week course graduates strike fighter tactics instructors who return to fighter squadrons to train fellow aircrews in air - to - air and air - to - ground tactics

    在從為期10周的訓畢業之後,斗攻擊員將回到他們的中隊對同伴進行術和術的訓
  3. Compared with a delta wing aircraft, the double - delta wing configuration has better aerodynamic performance at high angles of attack. an operational analysis was introduced as a method for evaluating training effectiveness of trainer aircraft. approaches to the engineering estimation of aerodynamic characteristics for aircraft with a double - delta wing configuration were studied, and the procedures for determining aircraft performance indices formulated. taking training effectiveness as the objective function and geometric parameters of the wing platform as design variables, through a numerical multivariate optimization arithmetic, the conceptual design optimization for a certain fighter trainer aircraft with double - delta wing configuration was carried out under the constraints of tactical and technical requirements and interrelated geometry. agreement of a calculation example with engineering practice indicates that the optimal design has higher training effectiveness than the baseline design, and in addition, improves the structural force - bearing conditions

    雙三角翼氣動布局比三角翼飛具有更好的大攻角氣動力特性.引入了評估效能的作分析法,研究了雙三角翼布局飛氣動力特性的工程計算途徑以及飛性能指標的確定方法.以訓效能作為目標函數並選取翼平面形狀的幾何參數為設計變量,採用多變量數值尋優方法,在術技術指標及相關幾何約束條件下,對某高級的雙三角翼氣動布局方案進行了優化選擇.算例表明最優方案不僅比原準方案具有更高的訓效能,還改善了結構的受力情況,與工程實踐吻合
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