翼間的 的英文怎麼說

中文拼音 [jiānde]
翼間的 英文
interplane
  • : 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...
  • : 間Ⅰ名詞1 (中間) between; among 2 (一定的空間或時間里) with a definite time or space 3 (一間...
  • : 4次方是 The fourth power of 2 is direction
  1. Cyclobutane exists predominantly in a "butterfly" conformation, in which the dihedral angle between the two wings is about 20°。

    環丁烷主要成「蝶式」構象存在,其中兩翼間的二面角大約為20。
  2. She moved cautiously along the entry.

    她小心地出了套門。
  3. The initial retrofit consisted of removing the gaps between the stringer flange and floor beam by providing shims.

    最初修復工作是通過墊片來消除縱梁緣和橫梁之隙。
  4. The first tetrapods, or land - living vertebrates, appeared during the devonian, as did the first terrestrial arthropods, including wingless insects and the earliest arachnids which had already ventured onto land during the silurian

    第一tetrapods ,或土地生存脊椎動物,出現在泥盆紀期,象第一地球節肢動物,包括已經冒險土地在西里瑞斯人期昆蟲和最早期蜘蛛綱動物。
  5. The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation

    本文主要研究是傾轉旋飛行器懸停狀態時,旋氣動干擾問題。
  6. When the tilt rotor vehicle is in hover, the aerodynamic download of the rotor flowfield imposes on the wing. in this time, the rotor / wing interaction is severe

    傾轉旋飛行器懸停時,旋下洗流剛好作用在機上,此時,旋翼間的氣動干擾非常劇烈。
  7. In her spare time, sharon loses no time in better equipping herself. to know more about flying, she has taken a course on fix - wing aircraft. this is also helpful to her job

    在工餘時,劉女士積極進修,參加了定駕駛課程,加深對駕駛飛機認識,這對她工作亦有幫助。
  8. And in spite of that, his attitude to hersolicitous, tender, and lovingwas so far from being changed, that he seemed overjoyed indeed that now a sort of kinship between him and princess marya allowed him to give freer expression to his loving friendship, as princess marya sometimes thought it

    不過,雖然如此,他對她態度小心,溫柔,殷勤不僅沒有改變,而且他似乎還高興,現在他與瑪麗亞公爵小姐之親戚關系,使他能更自如地對她表示自己友情與愛心,瑪麗亞公爵小姐有時這樣想。
  9. Then an thorough computer modeling using finite element program with material, geometry and state triple - nonlinear taken into account is carried out on a series of influencing factors, such as comparison with npn - beam splice connection, comparison of varies designed theories, and the varying of fraction coefficient, diameter, grade, pretension and arrangement of bolts, thickness of web and flanges of beam and column, splicing location, axial loading on column, etc. lots of useful conclusions are drawn form computer modelling. finally, design and construction suggestions are given out. this study fills the black in the field of steel beam - to - column connection with cantilever beam high - strength bolted - splicing at both home and abroad

    然後,本文在考慮材料、幾何和狀態三重非線性基礎上,對該連接形式進行了全面計算機模擬,主要考慮了帶懸臂梁段全螺栓拼接樑柱連接節點與無拼接樑柱連接及緣對接焊接腹板拼接連接節點對比,各種設計方法之對比,以及緣拼接和腹板拼接螺栓距、直徑和數量,拼接點與梁端之距離,梁和柱緣、腹板厚度,柱軸力,接觸面摩擦系數,緣和腹板拼接板厚度等因素影響。
  10. Her appearance belongs to the fire type, has sharp type of face, there are more black than white in the pupils of her eyes, both eyes are wide apart, the ears are lower than the eyebrows, her earlobes are thick and broad, protruding internal earbone, short nose, wing of the nose is frail and a little protruding, her mouth forms a line when it is closed, the sides of her mouth is slightly turn downwards, the thickness of the upper and lower lips is even, her cheekbones are not high, and the law grain is profound

    面相屬火,尖形臉,額頭高且突,下巴尖,眼珠黑多白少,兩眼距離開闊,眉陵骨凸,耳低於眉,耳珠厚和寬,內耳骨凸出,鼻短、鼻單薄和有點外仰,人中平滿欠缺凸下溝紋,嘴巴緊閉時成一線,嘴邊兩角微微向上彎,上下唇厚度均勻,顴骨位置不高也不大但法令紋深長。
  11. Furthermore, because rotors are mounted on the tips of the wing, the rotor / pylon / wing aerodynamic interactions are also included in the model. such factors reflect the unsteady and nonlinear characteristics in the model

    此外,傾轉旋飛機安裝在尖,旋/發動機短艙/機氣動干擾是建模一個難點。
  12. 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頭部,初級飛羽和上淡灰色強烈對比,以及七枚帶黑色初級飛羽
  13. This paper applies nonlinear finite element program bsnfem to analyze the behaviors of eccentrically braced steel frames under cyclic load. the study that comprehensive and systematic analyze the factor of links length, thickness of links flange, distance of links rib, thickness of links rib and angle of brace to be changed affect energy - dissipation capacity of d shape and k shape eccentrically braced steel frames have been some studied before. this paper fills the black in the filed factor of high - span ratio, brace stiffness and brace - to - beam connections to be changed affect energy - dissipation capacity of d shape and k shape eccentrically braced steel trames and any factor to be changed affect energy - dissipation capacity of y shape eccentrically braced steel frames

    對耗能梁段長度、耗能梁段腹板厚度、耗能梁段厚度、耗能梁段加勁肋距、耗能梁段加勁肋厚度、支撐夾角等因素改變對d形、 k形偏心支撐鋼框架耗能影響,前人已有一些研究,本文對這些因素影響進行了全面系統分析,完善了理論分析不足;而結構高跨比、支撐剛度、支撐與梁連接形式等因素對d形、 k形偏心支撐鋼框架破壞機理研究以及各種因素對y形偏心支撐鋼框架破壞機理影響,則很少有人涉及,本文對此也進行了深入系統分析,填補了這一研究空白。
  14. 962m respectively ). neighbouring segments are linked with bolts and welding. after the girders were segmented, guesseted plates were used with high - strength bolted oints to connect the web plates, and the higher and lower flange plates were butt - welded

    相鄰梁段之連接形式為栓焊混合型連接,採用節點板把腹板用高強螺栓連接後上、下緣板分別對焊。
  15. At the end of this section the paper specifies three possible failure modes of the ultimate resistance, depending on the ratio between the flexural resistance of the flanges and the axial resistance of the bolts. this numerical analysis includes many nonlinear structure behaviors such as contact status nonlinearities, geometric nonlinearities and material nonlinearities

    文章就連接緣板剛度變化和設置加勁肋等構造措施對連接高強度螺栓內力、緣板接觸壓力、撬力和節點剛度影響進行了對比分析,並對有限元計算結果進行了多項式擬合。
  16. Based on the mechanism of slipstream interaction, described in this thesis is firstly the interaction of the propeller slipstream with the wing 、 fuselage and horizontal tail. subsequently, the changes in lift 、 drag and pitching moment are derived, giving an engineering model for the prediction of the increments in the aerodynamic characteristics caused by the interference between the propeller slipstream and the other parts of aircraft. this method offers a powerful means to the calculation of the aerodynamic interaction between the propeller and the aircraft, providing reliable data for the design of and aerodynamic calculation on propeller - powered aircraft

    本文以滑流干擾機理為出發點,研究了螺旋槳滑流與飛機機、機身、平尾組合體之相互影響,推導出滑流引起飛機升力、阻力和俯仰力矩變化,給出了滑流干擾對機體氣動特性影響工程估算方法,為研究螺旋槳與飛機部件之相互干擾提供了有力工具,為以螺旋槳發動機為動力飛機設計和氣動計算提供可靠依據。
  17. The additional fins on either side of the nosecone ( 2 ) now have a wing - shaped profile, which improves airflow efficiency between the chassis and the tyres

    鼻錐兩端小鰭( 2 )現在有了外觀,可以增進車架和輪胎之氣流效率。
  18. After the data is analyzed, the software of fluent is used to calculate the flowfield. in order to make the calculation results agree with the experimental data, the model of the calculation has been modified based on the results of the experiment data

    詳細分析比較旋翼間的氣動干擾試驗數據后,應用fluent軟體進行分析計算,根據試驗結果修正計算模型,使計算結果與試驗結果趨於一致。
  19. 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優先請求更改破風車隊,寶馬薩伯修正了尾側板和主要外形,襟翼間的接合處。
  20. In order to understand the rotor / wing interaction each other, firstly, the change of the isolate rotor thrust with the collective pitch and rotate speed is tested, secondly, the change of the rotor thrust with the collective pitch, rotate speed and the wing / rotor distance is scaled, when the wing is placed underside the rotor, lastly, the pressure on the wing due to the rotor wake is scaled

    為了搞清楚它們之相互影響,本文首先測量孤立旋拉力隨總距和轉速變化;再測量有機時旋拉力隨總距及轉速變化以及隨旋翼間的距離變化;最後測量旋尾流對機表面壓力影響。
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