wing edge 中文意思是什麼

wing edge 解釋
翼緣
  • 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...
  • edge : n 1 刀口，（刀）刃；鋒；端；銳利。2 邊，棱，邊緣，邊界，界線，界限。3 優勢，優越條件。4 （聲調、...
  1. Fracture analysis of joint pole for front edge wing on boeing 735 - 500 plane

    500飛機前緣襟翼操縱連桿斷裂分析
  2. For hang gliders, to keep the parachute away from the wing, the bridle must extend past the hang glider ' s leading edge

    對懸掛滑翔機而言，連接帶的長度必須跨過前緣，這樣的後果是增加了備份傘的穩定性和降低了下沉率。
  3. Much more increase of maximum lift - to - drag ratio can be obtained with a forward - swept main wing with a small sweepback angle leading edge

    主機翼前掠角較小時，鴨翼改善和提高陞阻比的效果比較明顯。
  4. Numerical investigation of the effects of different leading - edge profiles on vortical flows over a double - delta wing

    尖頂襟翼長度對三角翼前緣渦破裂的影響
  5. The effects of trailing edge jets on the vortex breakdown of a delta wing

    后緣噴流對三角翼前緣渦的影響
  6. The effects of vectored jet on leading edge vortex breakdown of 65 176 ; delta wing

    矢量噴流對65 176 ;三角翼前緣渦破裂的影響
  7. 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
  8. Abstract : the effects of airfoil geometric parameters on wing " s spacial and polarized scattering characteristics have been systematically revealed. the results of the study indicated that the calculating value of diffraction from trailing edge by using the formula of the straight wedge is very far from experimental results for vertical polarization, and the contribution of thickness of the trailing edge to scattering must be considered in the calculation. the scattering peak of leading edge depends only on radius of airfoil for horizontal polarization. but for vertical polarization, it depends on maximum thickness and the location of maximum thickness. engineering formulas for evaluating all scattering peaks were given in the paper. it is important for the design of low - rcs wing

    文摘:系統地揭示了翼形幾何參數對機翼的空間散射特性、極化散射特性的影響規律.研究發現，在垂直極化狀態下用理論尖劈公式計算機翼后緣繞射的計算結果與實驗結果相差甚遠.提出在垂直極化狀態下機翼后緣繞射的計算必須將后緣厚度考慮在內的見解.對於水平極化，前緣散射波峰只與前緣半徑有關；而對於垂直極化，前緣散射波峰與翼形最大厚度以及最大厚度位置有關.給出前後緣散射波峰的工程估算公式，為低雷達散射截面（ rcs ）機翼設計提供依據
  9. A variable control surface on the trailing edge of an aircraft wing, used primarily to increase lift or drag

    襟翼飛機后翼上最初用來增加上升力或拖力的可靈活控制的輔助翼
  10. I touch by the edge of the far - spreading wing of my song thy feet which i could never aspire to reach

    我的歌兒展翅，那遠伸的翅梢，觸到你的雙腳，這是我從未渴望過的。
  11. The receiver aircraft is fitted with a probe that extends out from the side of the fuselage or from the leading edge of the wing

    受油機裝備有一個從機身一側或者是機翼前緣伸出的探頭。
  12. The only evidence would be any recordings where radar approach states that they see nothing on radar ( no evidence ) and all the paint and fiberglass missing from the leading edge of my outer port wing ( still no evidence )

    唯一的證據會是雷達接近地方的任何記錄，在雷達上什麼也沒看見（沒有證據） ，也絲毫看不見我外面的艙門機翼（也沒有證據）螺旋槳的前緣所失去油漆和玻璃纖維。
  13. Experimental studies on leading - edge vortex breakdown and control of flow over 76 176 ; 40 176 ; double delta wing

    雙三角翼前緣渦破裂及其控制實驗研究
  14. According to the theory of boundary layer control and aerodynamics of delta wing at medium attack angle, the generation mechanisms of rolling, pitching, yawing moments, which are produced by coupling between the microactuator array and boundary layer near the leading edge, have been discussed

    首先，結合空氣動力學的邊界層控制原理以及三角翼在中等攻角條件下的氣動特徵，詳細討論了微致動器陣列通過與前緣邊界層的耦合產生三角翼翻滾、俯仰和偏航等力矩的機理。
  15. 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。
  16. Experimental investigation for the effects of vectored trailing - edge jets on the leading - edge vortex reakdown of a double delta wing

    雙三角翼前緣剖面形狀對渦運動的影響
  17. With outstretched wings five cubits wide ; the distance from the edge of one wing to the edge of the other was ten cubits

    這一個基路伯有兩個翅膀、各長五肘、從這翅膀尖到那翅膀尖、共有十肘。
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