vertical tail 中文意思是什麼
vertical tail
解釋
垂直尾翼-
Double - wing micro air vehicles adopts the aerodynamic shape : no tail, only wings and vertical tail placing in wing
雙翼式微型飛行器採用無尾式，且只有機翼，垂尾也置於機翼上的氣動布局。 -
The active vibration control aimed at aircraft empennage has huge practical values in the aspects of adding the fatigue life of vertical tail, increasing the capability and availability of the aircraft, reducing the through - life - support costs and so on
飛行器垂直尾翼的振動主動控制對于提高尾翼的疲勞壽命、飛行器的機動性以及減小飛行器的維護成本具有較大的實際意義。 -
Hawk both feet stress one number of people each, number of people eyebrow is it erect to take place or after the vertical brain, this pattern, theme any meaning, is it study to worth also, to chisel engineer to be very much ingenious even jade wearing this, hawk eye, body, tail with latent to get up pair collude open line tick outline, feather is it adorn to carve with overcast line, seem vivid
雄鷹氣宇不凡，雙眼瞪圓，昂首引頸，展翅欲飛，頭上的肉冠極長，一直披到翼。鷹雙腳各抓一個人頭，人頭眉發豎立或垂直腦后，這一圖案，主題是什麼涵義，還值得研究，此玉佩的琢工也很巧妙，鷹目身尾用隱起雙勾陽線勾出輪廓，羽毛用陰線刻飾，顯得生動。 -
The november 12 crash of flight 587 in new york city, in which the tail fin, or vertical stabilizer, of an airbus a300 fell off, raised concerns about the increasing use of composites over metal
去年11月12日在紐約市墜毀的587號班機，是由於該架a300型空中巴士的尾翼，或稱垂直平衡器，從機身脫落所致；因此有關復合材料日益取代金屬的使用情況，引起大眾關切。 -
The vertical tail size is not set to avoid spiral instability because this mode is not critical.
垂尾的大小不是根據避免螺旋不穩定來確定的。因為這種運動模態不是設計狀態。 -
Discussions on dust removal for tail gas of vertical lime kiln of guangzhou iron amp; amp; steel group jinshi branch
廣鋼金石分公司石灰豎窯尾氣除塵探討 -
The wind - tunnel investigation of the characteristics and mechanism of twin - vertical tail buffet of leading - edge extension configuration
邊條翼布局雙垂尾抖振特性與機理風洞實驗研究 -
Optimal design of vertical tail using genetic - neural network algorithms
神經網路演算法優化飛機垂尾 -
The sideslipping airplane gives rise to a side force on the vertical tail.
側滑的飛機在垂直尾翼上引起側力。 -
When pilots attempted to maneuver with the tail ' s rudder in the wake turbulence from a preceding aircraft, the entire vertical stabilizer separated from the airplane, sending the a300 into a death spiral
當飛機碰上由前一架飛機所殘留的亂流，機長試圖操縱尾翼的方向舵時，就造成整個垂直平衡器與機身分離，也使得那架a300飛機?旋直下，邁向死亡。 -
Meanwhile, the soft of measured load calculation based on strain method and the soft of theory calculating load on vertical tail are programmed by fortran language
採用fortran語言編制了應變法實測載荷回歸計算程序，垂尾載荷理論計算程序。 -
The material characteristic and principle of piezoelectric material ( pzt ) and macro - fiber composite ( mfc ) is analyzed. cada - x structural dynamics analytic software is used to carry on the experimental modeling and mode analysis of the vertical tail. consequently, the disposal scheme of sensor and actuator is confirmed
本文的主要研究內容為:一、分析了壓電陶瓷和壓電纖維復合材料的特性及工作原理，採用比利時lms公司的cada - x結構動力學分析軟體對尾翼模型進行實驗建模與模態分析，根據模態實驗結果，確定了傳感/驅動元件的布置方案。 -
The vertical tail is less affected by the remainder of the airplane.
垂尾受飛機其它部分的影響較小。 -
This paper aims at model of vertical tail based on certain type aircraft. the method of distributed actively vibration control based on multi dsp has been carried on this model. a distributed actively vibration control system based on dsps is designed to real timely control the structural vibration of two modes
本文以某型飛機的尾翼模型為目標，採用基於多dsp處理器的分散式控制方法實現對垂直尾翼模型的振動主動控制，開發出了一套基於dsp的振動主動控制系統，針對結構的兩階模態振動實施了分散式振動主動控制，並進行了相關的理論和實驗研究。
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