翼部面 的英文怎麼說

中文拼音 [miàn]
翼部面 英文
wing section
  • : Ⅰ名詞1 (翅膀) the wing of a bird 2 (像翅膀的東西) the wing of an aeroplane etc : 鼻翼 wing of...
  • : Ⅰ名詞1 (部分; 部位) part; section; division; region 2 (部門; 機關或組織單位的名稱) unit; mini...
  • : Ⅰ名詞1 (頭的前部; 臉) face 2 (物體的表面) surface; top 3 (外露的一層或正面) outside; the ri...
  1. There are more than one hundred natural and artificial sights in jiangjin, forming a traveling netwlrk with a line along the yangtze, a south wing of simian mountain, and a north wing of beicao mountain water ? eroded cave sights group. it has become an important part of chongqing tree gorges traveling hotline

    江津境內有100餘處自然和人文景觀,形成了以長江沿線景觀為一線,四山為南,碑槽山溶洞風景群為北的「兩一線」旅遊網路,是重慶三峽旅遊熱線的重要組成分。
  2. Based on basic principles of grillage method, an improved grillage model of wide cantilevers bridge deck is brought forth and its effectiveness is verified after generalizing rules of grillage meshing and sectional characteristic

    基於梁格法的基本原理,提出了寬緣上結構分析的改進梁格模型,並總結了梁格單元劃分和截特性計算的一般方法,最後通過算例驗證了該模型和方法的有效性。
  3. The bottom edges of the endplates are mated to another winglike device, the lower main plane, which in turn is attached to the rear crash structure ? a carbon fibre cone bolted onto the gearbox

    終板末端邊緣被設計成與另一個狀地設備相配合,這個狀設備是一個較低的平,附著在尾碰撞結構上? ?變速箱上的碳纖維錐形螺釘。
  4. When attacking you should aim to take advantage of flanking, for example using shock troops blinking behind units and delivering hits in the rear

    在攻擊時,你應該著眼于獲得側優勢,比如用你的震波隊瞬移到敵人後,從背後襲擊它們。
  5. Well hidden by the winglet / chimney combination, they dramatically improve hot - air extraction from the sidepods, allowing the engineers to lower the rear section of the car, including the exhaust

    它們被很好地隱藏在小/風道組合件的下,可以極大地改善吸取來自於側箱的熱空氣,讓工程師們可以降低賽車的尾,包括排氣管。
  6. Pull the servo extension cord out of the middle hole above the wing, for later use

    舵機延長線從機的孔中用預留的線繩拉出備用。
  7. In the region of investigation, the water in the soil is upward and under the evaporation condition in the first zone, where intensive evaporation occurs ; the matrix potential of soil water is downward so that the water is downward in the second zone

    在研究區內,第一個分帶是水分向上運動,水分處于蒸發狀態,常年處于極度乾燥狀況;第二分帶水土勢較低,也就是第一個零通量的下分,在這一分帶中水分向下運動。
  8. Easy freight counts as it s third advantage : remote controllable airboat is made up by several parts gasbag, suspending house and tails, it has a small volume when no flying, can be freighted by a small car, a middle shift can carry evething including operaters and gas bottle, to implement a multi - days, multi - places flying

    運輸簡便是它的第三大優點遙控飛艇是由多個件拼裝在一起的分為氣囊吊倉和尾三大分,不飛的時候體積很小,一輛夏利或小的就可拉走,一輛中巴可連人員帶氣瓶帶飛艇全拉走,進行多日多地點的行動飛行。
  9. The interior temperature distribution and ablation model of projectile wing is established from general transmitting heat differential equation ; at the same time, the heat flow density and pressure distribution model of projectile wing is also established

    從一般形式的導熱微分方程出發,逐步建立了彈溫度分佈和燒蝕的數學計算模型;與此同時,建立了彈的熱流密度和壓力分佈的數學模型。
  10. A part or surface, such as a wing, propeller blade, or rudder, whose shape and orientation control stability, direction, lift, thrust, or propulsion

    ;機一個件或平,如機、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
  11. Mongolian gull : pale upperside, clear contrast between black primaries and pale blue - grey upperwing, strikingly white head, typically two quite large mirrors on p10 and p9

    蒙古銀鷗:淡色的上,黑色初級飛羽和淡藍灰色上間明顯的對比,顯著的白色頭,典型地在p10及p9上有二個相當大的
  12. Vega gull : pale upperside, clear contrast between black primaries and pale grey upperwing, dirty head ( may be almost hooded, with very heavy, wide, blob - shaped brownish marks ), more rounded wing, some have bright raspberry - pink legs

    織女銀鷗:淡色上,黑色初級飛羽和淡灰上間明顯的對比,污色的頭(可能幾乎罩住頭頂,非常深,寬,點狀的棕色斑點) ,比較圓弧的翅膀,有些有明亮的覆盆子般粉紅的腳
  13. As is well known, the effective width depends on several factors, such as the cross - section width, the height of web, the spacing of span and so on. we can conclude that width / span ratio ( overhang width / span and central width / span ) is the governing factor of the effective width

    影響箱形截樑上緣有效寬度的因素很多,如上緣寬度、梁高、跨度以及結構體系等,通過大量計算表明寬跨比[分寬度、箱室分寬度與跨度的比值]是有效寬度的控制影響因素。
  14. The bird is normally 46 - 59 cm in length, but the overall size and body proportions vary regionally. generally, all forms have dark greyish plumage from the back of the head, neck, shoulders and lower body. their wings, tail, face and throat are glossy black

    這種鴉通常身長四十六至五十九厘米,實際體積和身體比例隨不同地區而各異,但羽毛均為灰黑色,、尾、頰和喉尤其漆亮。
  15. 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分:半導體器件包裝用表安裝略圖制備的一般規則.鷗型引線終端的設計指南
  16. Nikolay recognised princess marya at once, not so much from the profile he saw under her hat as from the feeling of watchful solicitude, awe, and pity which came over him at once

    尼古拉立即認出瑪麗亞公爵小姐,他認出她與其說是憑她帽子下露出的孔側的輪廓,不如說是憑那種謹慎恐懼和憐憫感情,這種感情馬上支配了他。
  17. A second method is to furnish the surfaces with hinges and to use an exterior sector with drilled holes for each angle setting.

    第二種方法是在上裝置鉸鏈,用一個對不同安裝角鉆有不同孔的外扇形件與之配合。
  18. This one mongolian with white head, strong contrast between primaries and pale grey of upperwing and seven black - marked primaries

    這只蒙古銀鷗有白色的頭,初級飛羽和上的淡灰色間的強烈對比,以及七枚帶黑色的初級飛羽
  19. Firstly, the paper analyzes the basic airfoil profile in theory. its forepart adopts ellipse column shape and its back - end adopts plane shape. simultaneously, the 3d parametrizing model is set up

    首先,本文是從理論上對基準型進行了分析,前段曲線分採用橢圓柱結構,后緣分採用平結構,建立了飛機機的三維參數化模型。
  20. In order to predict hydrodynamic characteristics a computational system is developed including determination of the pressure distribution on a wing section by use of the conformal mapping method and panel method respectively and of the flow in boundary layer according to the thin shear layer approximation ( tsl ) for navier - stokes equation approach. the wing sections of naca4412 and naca0012 are applied to test the computational system. the numerical inspection shows that the panel method with better precision and the momentum and the displacement thickness of boundary layer can be used to complete this calculation

    本文分別用守屋的保角變換法和基於源匯渦分佈的元法,建立了計算槳葉表壓力分佈的數學模型;應用納維-斯托克方程的薄層近似理論模式和有限差分數值方法,建立了計算機邊界層內流動的數學模型;應用槳葉表邊界層內粘性流動和外勢流流動在邊界上的匹配演算法,建立了槳葉表二相流流動的計算方法和相應的計算機程序。
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