wing surface 中文意思是什麼

wing surface 解釋
翼表面
  • 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...
  • surface : n 1 表面；地面；水面；廣場，空地。2 外觀，外表，皮毛。3 【幾】面；切口；【航空】翼面。adj 表面的...
  1. If this load centroid is behind the elastic axis of the wing structure, then a nose-down twist of the main wing surface results.

    如果該載荷重心在機翼結構彈性軸之後，則引起主機翼表面前端向下的扭轉。
  2. Wing - in - surface effect crafts belong to a class of transport vehicles, which make use of the ground effect to fly

    地效飛機是一種主要利用地面效應提供支承力而飛行的運載工具。
  3. Abstract : wing - in - surface effect crafts belong to a class of transport vehicles, which make use of the ground effect to fly

    文摘:地效飛機是一種主要利用地面效應提供支承力而飛行的運載工具。
  4. Within the field of ground effect, aerodynamic forces of the wing - in - surface effect crafts are not only decided by the angle of attack, but also by the flying height, and they lead to more complicated stability problems

    在地效作用區域內，地效飛機的氣動力不僅與迎角有關，而且與飛行高度有關，因而其飛行穩定性問題更為復雜。
  5. Firstly, a representative wind and wave model, which could both simulate the main characteristics of wig over sea waves and be suitable for numerical calculation, is presented. the model completely considers the fully nonlinear effect of wave surface on the wavy air flow, separates the disturbance of wave surface from the wing - air wave interaction flow, and overcomes the numerical calculation difficulties due to the large difference of dimensions between wing and water waves

    首先針對機翼在風浪中的非定常非線性氣動力問題，提出了一個既能夠反映風浪場主要特徵又適合於數值計算的風浪場模型，該模型完整地考慮了波浪表面對氣流場的全非線性影響，使波面對流場的擾動分離出來，消除了機翼和波浪幾何尺度上的巨大差異帶來的數值計算上的困難。
  6. A part or surface, such as a wing, propeller blade, or rudder, whose shape and orientation control stability, direction, lift, thrust, or propulsion

    翼剖面；機翼；翼面一個部件或平面，如機翼、螺旋槳葉、方向舵等，其形狀或方位控制穩定性、方向、抬升、沖擊或驅動
  7. These advantage make it excellent materials for control surface, wing and skin of airplane

    是飛機結構中對剛度要求較高的操縱面、機翼和機身蒙皮結構用較理想的材料。
  8. Coil tightly the stainless steel radiator wing around the electric heating pipe to enlarge the radiating area of the heating tube surface and the heater radiates more quickly, have higher heat use rate and the power density of the heater will be improved. structure sketch

    分體機用翅片加熱器，是電加熱管上緊密繞制不銹鋼散熱翅片，它增大了加熱器表面的散熱面積，使加熱器散熱更快，熱利用率更高。
  9. Mechanical standardization of semiconductor devices - part 6 - 1 : general rules for the preparation of outline drawings of surface mounted semiconductor device parkages - design guide for gull - wing lead terminals

    半導體器件的機械標準化.第6 - 1部分:半導體器件包裝用表面安裝略圖制備的一般規則.鷗型翼引線終端的設計指南
  10. The surface finite element solver brought forward by woodward is improved. according to the improved solver, the interfere between bomb and plane is researched. the aerodynamic parameters of the bomb, which under the wing are calculated

    本文對伍德沃德提出的面元法加以改進，並應用改進后的面元法對航彈機彈干擾進行了研究。
  11. 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
  12. Three models are employed to analyze the aerodynamic characteristics of a wing above sea - wave. those are ( 1 ) curve surface effect ( c. e. ), ( 2 ) wavy air motion effect ( w. e. ) and the coupled effect a. e

    研究了曲壁面效應，波動效應以及壁面和波動綜合效應三種影響模式對二維和三維機翼在風浪中飛行時的氣動力性能的影響規律，指出了二維和三維機翼氣動力特性的共性和區別。
  13. Mechanical standardization of semiconductor devices - general rules for the preparation of outline drawings of surface mounted semiconductor device packages - design guide for gull - wing lead terminals

    半導體器件的機械標準化.表面安裝的半導體器件封裝外形圖繪制的一般規則.海鷗翼式鉛端子的設計指南
  14. Mechanical standardization of semiconductor devices - part 6 - 1 : general rules for the preparation of outline drawings of surface mounted semiconductor device packages ; design guide for gull - wing lead terminals

    半導體器件的機械標準化.第6 - 1部分:平面式安裝半導體器件外殼外形圖繪制的一般規則.海鷗翼式鉛終端的設計指南
  15. We generated its grid surface on the fuselage or missile body according to the geometry projection relation between aerodynamic components and the bilinear interpolation approach. finally, we successfully developed a new algebra grid generation technique in virtue of the improved four - boundary interpolation. in this thesis, we put emphasis on the researches of aerodynamic inverse design and drag reduction questions for airfoil and wing using euler equations and control theory proposed by jameson

    （ 2 ）進行了應用控制理論和二維歐拉方程的翼型氣動反設計，以及有升力約束情形下翼型跨音速減阻問題研究，分別推導了相應的共軛方程及邊界條件的數學形式，並給出了相應的梯度求解公式形式，研究發展了共軛方程及梯度的數值求解方法，成功進行了多個翼型的反設計和減阻問題研究。
  16. Firstly, itis explained that the application research of smart layer. to laod detecting and simulative damage for the model of wing - box, fbg fiber smart layer and pzt smart layer are designed, and manufactured. so, those are surface - mounted respectively on the stiffened skin of aluminum alloy and carbon fiber reinforced. data acquisition system based on different signal processing technique are designed

    針對機翼盒段試件結構載荷識別和模擬損傷監測的功能要求，結合智能夾層的設計製作工藝，設計製作了基於fbg傳感器的光纖和壓電兩種智能夾層，並分別安裝在機翼盒段試件上的鋁合金和碳纖維制蒙皮上。
  17. Firstly, this paper gives an introduction about wing - in - surface crafts and their development state so far, then analyzes and describes their special stability and control problems, at last presents an outlook about their application perspectives

    首先介紹了地效飛機的一般特點和發展現狀，然後分析和描述了該類飛行器特有的穩定性問題以及控制特點，最後展望了它的應用前景。
  18. As a class of nonlinear multivariable objects, which characteristics is difficult to identify, the wing - in - surface effect crafts need adopt more complicated control laws and integrated information - control systems to ensure the flight safety and control efficiency

    作為一類非線性、多變量且很難辨識的受控對象，地效飛機應採用更加復雜的控制律和信息? ?控制綜合系統，以最大限度地保證低高度的飛行安全和操控效率。
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