tail lift 中文意思是什麼

tail lift 解釋
尾翼升力
  • tail : n 1 尾巴。2 尾狀物，垂下物；（西服的）垂尾，燕尾；〈pl 〉燕尾服。3 辮子；風箏尾巴。4 末端；結尾，...
  • lift : vt 1 舉起，使升起，提起，抬起；提高；提升。2 使高尚；鼓舞。3 運送，搬運；空運 （ ＝ airlift） 4 ...
  1. Introduce according to the relevant data, persian cat is in around 16 centurieses, from the himalayas cat and angola cat miscellaneous hand over, lift through several years to breed but grow purely. persian cat ' s figure is bigger, wering grown by the hair and thick and airtight, head circle big, the face is flat even, sum breadth the ear is small, circle the eye snub - nosed tone short breadth, the body feels round and smooth because the hair grows, the arms and legs is thick short soft, the tail is fluffy and bulky, giving person a kind of noblest felling. persian cat ' s pressing is canned is divided into a white, black, red by the hair color ' s dissimilarity, yellow, dark gray, blue, double color, tortoise shell color, miscellaneous color, tiger spot color etc. species. take species of the red as among them valuable

    根據有關資料介紹，波斯貓是在16世紀左右，由喜馬拉雅貓和安哥拉貓雜交，經過多年的提純繁殖而培育出來的.波斯貓體形較大，被毛長而且厚密，頭圓大，臉扁平，額寬耳小，圓眼塌鼻口吻短寬，軀體因毛長而感覺渾圓，四肢粗短柔軟，尾蓬鬆粗大，給人一種雍容華貴的感覺.波斯貓按被毛顏色不同可分為白色，黑色，紅色，黃色，暗灰色，藍色，雙色，玳瑁色，雜色，虎斑色等品種.其中以紅色的品種尤為名貴.波斯貓外表美麗大方，叫聲細小甜美，性格溫和，膽大好奇，喜歡與人親近，善解人意，容易調教，是一種深受人們喜愛的高貴寵物.有關波斯貓的起源眾說紛紜，現較統一的說法是在阿富汗土著長毛貓的基礎上，同土耳其或亞美尼亞地區的安哥拉貓雜交培育而成。
  2. The best glide speed varies with changes in lift / sink and wind conditions ( head / tail wind )

    最佳滑降比飛行速度（對空速度）改變經常取決于飛行傘上升率及沈降率或者是飛行傘順風、逆風飛行狀況。
  3. We are particularly awed by two of the orcas ' showstopper stunts when they spy hop ( lift their heads out of water to look ) and lob tail ( hit the surface with the underside of the fluke )

    這些虎鯨的兩項精彩絕技尤其令人震撼，也就是?們的浮窺（把頭抬出水面張望）和挑尾（用尾鰭底部拍打水面） 。
  4. Hiring of grab lorries and open covered lorry : item 1 - open covered lorry with tail lift and 2 labourers 1 aug. 2004 - 31 jan 2007

    租賃抓鬥貨車及開篷有篷貨車：項目1 -設有車尾升降臺的開篷有篷貨車及兩名工人
  5. 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

    本文以滑流干擾的機理為出發點，研究了螺旋槳滑流與飛機機翼、機身、平尾組合體之間的相互影響，推導出滑流引起的飛機升力、阻力和俯仰力矩的變化，給出了滑流干擾對機體氣動特性影響的工程估算方法，為研究螺旋槳與飛機部件之間的相互干擾提供了有力的工具，為以螺旋槳發動機為動力的飛機的設計和氣動計算提供可靠的依據。
  6. The kinematics mathematic model of lifting mechanism of vehical tail - lift is built by plural vector method

    摘要採用復數向量法建立了車用起重尾板起重裝置運動學的數學模型，分析了該舉升機構運動的特點。
  7. The tail lift curve slope as determined from the panel model may require adjustment in order to apply the test results.

    為了應用試驗結果，根據翼段模型試驗確定的平尾升力曲線斜率可能要作些修正。
  8. Hiring of 5. 5 - tonne gvw box - type single cab trucks with tail lift for hongkong post 1 sept. 2004 - 31 aug. 2006

    二四年九月一日至二六年八月三十一日
  9. Hiring of 5. 5 - tonne gvw box - type single cab trucks with tail lift for hongkong post 4 - hour hiring 1 dec. 2004 - 31 aug. 2006

    二四年十二月一日至二六年八月三十一日
  10. Hiring of 5. 5 - tonne gvw box - type single cab trucks with tail lift for hongkong post ( 4 - hour hiring ) 1 dec. 2004 - 31 aug. 2006

    二四年十二月一日至二六年八月三十一日
  11. Tail - lift for vehicle

    車用起重尾板
  12. A kind of grid generation method based on two - dimension poisson equtions is devlop - ed into the grid generation method based on three - dimension poisson equtions in this dessertation. use this method, this paper generals the grids of glide bullet to increase range that is at three states, that is with no control rudder and no tail wing, only with tail wing and with control rudder and tail wing. this paper has calculated the aerodynamic coefficients of glide bullet to increase range that is at three states. beside this the paper has given the results and analysised the differences of the three states, and the effects of control rudder and tail wing to the lift and drag. this can give us some information about the ability of the control ruder and tail wing for increasing the range

    本文在二維泊松方程網格生成方法的基礎上推導出了一種三維泊松方程網格生成方法。並利用該方法生成了繞彈體、尾翼彈、滑翔增程彈三種不同彈形的流場網格。計算了超音速來流下彈體、尾翼彈，滑翔增程彈三種不同彈形的空氣動力學系數，分析了三種不同彈形計算結果的差別；分析了控制舵和尾翼對升力和阻力的影響。
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