無尾翼的 的英文怎麼說

中文拼音 [wěide]
無尾翼的 英文
unfinned
  • : 無Ⅰ動詞(沒有) not have; there is not; be without Ⅱ名詞1 (沒有) nothing; nil 2 (姓氏) a surn...
  • : 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...
  • : 4次方是 The fourth power of 2 is direction
  • 尾翼 : [航空] tail surface; empennage; tail; tail assembly; tail fin; tailpiece
  1. Double - wing micro air vehicles adopts the aerodynamic shape : no tail, only wings and vertical tail placing in wing

    式微型飛行器採用式,且只有機,垂也置於機氣動布局。
  2. The flying stability of the unguided projectile with wrap around fins could be influenced by the self - induced rolling characteristics and the cross coupling effects of the waf badly. it is necessary to study further on this special aerodynamic problems

    卷弧存在自誘導滾轉特性、較嚴重交叉耦合效應等特殊氣動問題,對于卷弧彈而言,這很大程度上影響飛行穩定性。
  3. This paper has mainly made a research on the aerodynamic configuration design of " w " tailless aircraft and the design idea has been presented here. according to the configuration design requirement of certain uav, aerodynamic configuration design has been carried out and two configuration projects are given out at last : forward - swept wing tailless configuration and " w " tailless configuration. the longitudinal and lateral aerodynamic characteristics are obtained by using two aided soft : ug to build up geometrical models and mgaero to calculate flow field

    本文研究了「 w 」型布局氣動外形設計,闡述了該布局氣動設計思想,根據型人機總體設計技術指標,進行了氣動外形設計,提出了兩種氣動布局方案:前掠氣動布局和「 w 」型氣動布局,利用ug建模軟體和mgaero氣動分析計算軟體計算了兩種布局縱、橫向氣動性能,分析了前掠前緣掠角和身融合對氣動性能影響,計算結果表明, 「 w 」型氣動布局設計思想是正確,所設計「 w 」型氣動布局方案氣動性能優越,超過了總體設計技術指標。
  4. With his arms tied behind his back, he maneuvered himself to be able to remove the blindfold from me so i could untie myself then we all helped each other untie our feet to make a fast getaway. running as fast as our injuries allowed, we yelled and yelled, " we re americans ! we re americans !

    一天,我們坐在那裡,聽到有飛機飛來然後,是直升機低飛聲音然後,一枚炸彈從木屋頂丟進來,就落在我腳旁幾寸外,但它巴卻鉤在木屋頂上,離開了炸彈他們法相信,於是他們小心,把它拿下來。
  5. The design of configuration and other primary structures of the helicopter have been finished. in order to analysis the stability and control of the helicopter, a flight mechanical modeling has been founded based on a single - rotor helicopter

    本文以常規單旋直升機配平和操穩計算方法為基礎,建立了帶涵道共軸式直升機飛行動力學模型,對碟形人直升機進行了配平和操縱性和穩定性分析計算。
  6. Study on the impact of x - tail on static stability for an uav

    布局對人機靜穩定性影響
  7. Lastly, previous vane are analysed by fluent, we calculate the pressure distribution chart and report chart of each wing form, then alter the torsion angle and the airfoil form of the vane respectively, finally ascertain the influence curve of the torsion angle and the airfoil form of the vane on which act the lift power

    最後,通過fluent對設計出葉片分析,得出其壓力分布圖和報告圖。然後從改變葉片扭轉角度和型兩個方面分析其對升力和阻力影響。得出葉片扭轉角和型對升阻比影響曲線,在文章部分估算了人機一些性能參數。
  8. The peacock ' s tail stage - the conscious experience of the astral body - stands alone in this picturing of the process, though it was sometimes split into two facets, in the writings of some alchemists - an initial winged dragon phase which resolved into the peacock ' s tail

    孔雀巴狀態? ?星形身體意識體驗? ?獨一二地站立在這個過程描繪裏面,通過它不時地分裂出兩個刻面,在一些煉金術士作品裏面? ?最初有階段下決心進入孔雀巴。
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