特技飛行訓練 的英文怎麼說

中文拼音 [fēihángxùnliàn]
特技飛行訓練 英文
aerovatic training
  • : Ⅰ形容詞(特殊; 超出一般) particular; special; exceptional; unusual Ⅱ副詞1 (特別) especially; v...
  • : 名詞(技能; 本領) skill; ability; trick; technique
  • : 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...
  • : 行Ⅰ名詞1 (行列) line; row 2 (排行) seniority among brothers and sisters:你行幾? 我行三。where...
  • : Ⅰ動詞1 (教導; 訓誡) lecture; teach; train 2 (解釋) explainⅡ名詞1 (準則) standard; model; ex...
  • : 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...
  • 特技 : 1 (特殊技能) stunt; trick2 [電影] special effects特技場景 trick scene; 特技飛行 aerobatics; aer...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 訓練 : train; drill; manage; practice; breeding
  1. The intense ( 17 ) training of the pilots by patty wagstaff, a world famous aerobatic ( 18 ) pilot, and dale snodgrass, an expert aviation instructor

    員的魔鬼課程,是由兩位魔鬼擔任,一位是名員沛帝瓦格史朵夫,另一位則是專家戴爾史諾德葛萊斯。
  2. 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機具有更好的大攻角空氣動力性.引入了評估教效能的作戰分析法,研究了雙三角機翼布局機空氣動力性的工程計算途徑以及機性能指標的確定方法.以效能作為目標函數並選取機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,在戰術術指標及相關幾何約束條件下,對某高級教機的雙三角機翼氣動布局方案進了優化選擇.算例表明最優方案不僅比原準方案具有更高的效能,還改善了結構的受力情況,與工程實踐吻合
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