wing flap 中文意思是什麼

wing flap 解釋
襟翼
  • wing : n 1 翼,翅膀;鳥;鳥群;飛行,飛翔。2 (飛機)機翼;翼狀物;(汽車的)擋泥板;〈詩常 pl 〉船帆。3...
  • flap : vt ( pp )1 拍打,拍擊;拍動(翅膀),撲動。2 拍打(蚊、蠅等);使(帆、簾子等)拍動。3 把(帽邊...
  1. Effect of the apex flap on the leading edge vortex breakdown over a 70 176 ; delta wing

    尖頂襟翼對70 176 ;三角翼前緣渦破裂的影響
  2. General specification for indicator of wing flap position

    襟翼位置指示器通用規范
  3. Multi - gap - fowler - flap, while deflecting its rudders, simultaneously extends backwards by relatively large scope, which broaden the overall wing - camber and area, so that more additional lift could be attained through improving air - flow boundary layer

    多縫富勒襟翼在襟翼舵面偏轉的同時發生較大幅度的後退,增加機翼整體彎度和機翼面積,通過縫隙氣流改善附面層狀況,因而得到加大的升力增量。
  4. Through solving the unsteady flow fields of an airfoil - flap, the mechanism of buzz is intensively studied. on the basis of the unsteady flow fields of an airfoil - flap with an upper - wing spoiler, the mechanism of the upper - wing spoiler suppressing the buzz is researched. in additions, the comparisons of the unsteady flow fields of an airfoil - flap with and without a separator show that the separator reduce the speed of the buzz

    從非定常流場計算出發系統的研究了嗡鳴發生的機理以及擾流片對嗡鳴起抑制作用的機理;應用能量法確定了嗡鳴發生的邊界;並且研究了機翼舵面之間有隔膜和無隔膜以及機翼上有上翼擾流片和無上翼擾流片對嗡鳴發生邊界的影響;得出了有意義的結論。
  5. Numerical results show that the present method is effective one for solving the flow around wing with flap deflection

    數值算例表明本方法是求解帶襟翼偏轉的機翼繞流的有效方法。
  6. Look closely and you discover they are divided by a horizontal slit, in effect creating two tiny wing profiles, or a double flap

    靠近看你會發現他們被水平的狹縫分離,成為兩片小翼,或是雙層的襟翼。
  7. Compared with other types of the wing flaps, the effect of the fowler - flap generating more additional lift has great superiority, and so the multi - gap - fowler - flap has been used abroad for large or middle - scale cargo and transport airplanes

    它的增升效果與其它類型襟翼相比具有很大優越性,已經在國外許多大中型運輸機上得到應用。
  8. With the demands of designing the large - scale cargo airplane, in this thesis, many technical materials about the mechanisms of current wing flap types, of foreign transport airplanes are carefully studied at first, and the mechanical composition of three - gaps - fowler - flap is summarized technically about its major basic components, prime mechanism ( track ), driving device, sub - flaps mechanism and the sub - flaps sequential control system

    在本文中,針對大型運輸機機翼設計的需求,首先對幾種國外運輸機襟翼運動機構的資料進行仔細研究,對三縫富勒襟翼運動機構的組成進行了分析,總結歸納出了三縫富勒襟翼運動機構的3個基本組成部分:主機構(軌道) ,驅動機構,子襟翼機構及子襟翼運動控制機構。
  9. At present, the domestic development of large - scale cargo airplane is getting urgent, such that the design methodology of the mechanisms of fowler - wing flap must be investigated thoroughly as one of the critical technologies of developing large - scale cargo airplane

    目前國內航空工業的發展對大型運輸機的需求變得越來越緊迫,而研製大型運輸機的關鍵技術之一? ?富勒襟翼運動機構的設計方法? ?必須得到解決。
  10. Another team invited by the fia to make changes to their wings prior to australia, bmw sauber have revised the junction of the rear wing ' s endplates and its main profile and flap

    另一支在澳大利亞被fia優先請求更改破風翼的車隊,寶馬薩伯修正了尾翼側板和主要的外形,襟翼間的接合處。
  11. Fine, thank you. i discus the matter of those wing flap with my manager, and we will be

    很好,謝謝你。有關副翼的事,我跟我的經理商量過了,我們願意把價格降到每一件2 , 365 。
  12. Wing flap, widely assembled in various kinds of airplanes, can increase lift force rapidly in a short time, for an aircraft taking off or landing, and also at some emergency situations

    襟翼在各種飛機上普遍應用,它可以在短時間內增加飛機升力,主要用在飛機起降過程和特殊緊急情況下。
  13. The comparison of the computational results of flap movements indicates that three operational positions of the wing flaps guided through the different tracks are nearly close to each other and the non - arc - track is better to guide the flaps to the original three positions exactly

    計算結果表明,不同的軌道下所得的襟翼3個工作位置從幾何角度看比較接近,其中非圓弧軌道能夠使襟翼在3個工作位置與預先設計的姿態完全相同。
  14. A section of ( wing trailing - edge ) flap detached during flight probably due to material fatigue

    一段襟翼在飛行中掉落可能因材料疲乏。
  15. N - s method for solving the flow around a wing with deflection of flap is presented

    給出了帶襟翼偏轉的三維機翼繞流的一種求解n - s方程的計算方法。
  16. A n - s method for solving the flow around a wing with deflection of flap is presented

    給出了帶襟翼偏轉的三維機翼繞流的一種求解n - s方程的計算方法。
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