飛翼式飛機 的英文怎麼說

中文拼音 [fēiyìshìfēijī]
飛翼式飛機 英文
flying wing-type aircraft
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 翼 : 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...
  • 式 : 名詞1 （樣式） type; style 2 （格式） pattern; form 3 （儀式; 典禮） ceremony; ritual 4 （自然科...
  • 機 : machineengine
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  1. 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。
  2. None of the other p1 - lots present would have thought of going up, but hamel one of the finest of all pilots of the beriot monoplane was not to be stopped

    其他在場的飛行員都沒有想到要起飛，但是哈梅爾? ?這個布雷里奧式單翼飛機最優秀的駕駛員之? ? ?是不會被阻攔的。
  3. The model developed here is suitable for the tilt rotor aircraft during hover, transition and cruise. the longitudinal equations of motion provide a foundation for further investigation on tilt - rotor flight dynamics

    文中所建模型具有較高精度，適合於飛行包線內的所有模式，為傾轉旋翼飛機飛行動力學的進一步研究提供了基礎。
  4. Tilt - rotor aircraft combine the vertical takeoff and landing ( vtol ) capability of helicopters with the high speed performance of turboprop airplanes. located at the tips of the wing, the prop - rotors act as helicopter rotors when flying vertically and as airplane propellers in cruising flight

    傾轉旋翼飛機翼尖安裝可以傾轉的發動機短艙和旋翼系統，可以在飛行中根據需要在固定翼模式和直升機模式之間轉換，充分發揮直升機垂直起降、懸停及固定翼飛機高速巡航的優點。
  5. In this paper, the major subject investigated is the ducted fan vertical take - off and landing ( vtol ) uav. compared with normal fixed - wing uav, it has so many strong points such as be convenient to take - off and land, good adaptability and long hover time. we analyze and summary information of foreign uavs, then calculate the figure dimension of our uav, and draw the uav structure configuration and the outside view drawing of three dimensional structure

    本課題的研究對象是涵道風扇式垂直起落無人機，與一般的固定翼無人機相比，它有著起落方便、適應性強、可以在空中長時間盤旋等優點，本文通過對相關飛行器資料的分析總結，給出了無人機的大體結構尺寸，並畫出了無人機的結構布局圖和三維結構外觀圖。
  6. Such planes could fly to their destinations with the speed of their short wings, then extend their inflatables to burn less fuel while they loitered or slowed down for landing

    這麼一來，這類飛機可用較短的機翼提高速度飛到目的地，並在盤旋或減速準備降落時，拉長充氣式機翼，以減少燃料消耗。
  7. Three models are employed to analyze the aerodynamic characteristics of a wing above sea - wave. those are ( 1 ) curve surface effect ( c. e. ), ( 2 ) wavy air motion effect ( w. e. ) and the coupled effect a. e

    研究了曲壁面效應，波動效應以及壁面和波動綜合效應三種影響模式對二維和三維機翼在風浪中飛行時的氣動力性能的影響規律，指出了二維和三維機翼氣動力特性的共性和區別。
  8. 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

    本文以常規單旋翼帶尾槳的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，對碟形無人直升機進行了配平和操縱性和穩定性分析計算。
  9. Compared with the xv - 15 flight test data, the results are reasonable and effective. improved guidance schemes will be needed, especially in the terminal area for safety and economic viability

    傾轉旋翼飛機起飛過程包含完整的過渡模式，為提高飛機的可靠性和安全性，必須對其起飛軌跡進行控制。
  10. During the procedure, the airspeed continues accelerating ( or decreasing ) and the aircraft configuration is rapidly changing. the aerodynamic interactions are complex and lead to dynamic instabilities. the shift between helicopter and airplane flight modes necessitates a change in control strategy

    過渡模式下，飛機速度不斷增加（或減小） ，氣動布局不斷改變，飛機動力穩定性差且氣動干擾嚴重，直升機控制和固定翼控制切換，因此過渡模式動力學特性和控制系統研究是整個傾轉旋翼飛機研製的主要難點。
  11. Sonic fatigue stress simulation and pattern recognition of an aircraft flap

    飛機襟翼聲疲勞應力的模擬與模式識別
  12. This paper explored the micro pressure sensor that is used for the measurement of distributed pressure at the surface of smart - skin. firstly, established the surface pressure model according to the aerodynamic properties, defined the optical measurement system that based on intensity modulation principle, discussed the components of this system and theoretical analyzed its measurement theory in detail

    首先，根據空氣流動的基本規律給出機翼表面壓力分布圖，通過對光學式微型壓力傳感器的理論分析，採用強度調製法測量飛機機翼表面的壓力並建立基於此方法的光學測量系統模型，得到了壓力與敏感膜片變形以及光電轉換輸出能量之間的關系。
  13. Remote controllable advertising umbrella is our newly developed product, featuring stalbe flying, loudly sound, large advertising area, low flying speed, easily operation, no gas required, aluminum materialed wings, dispatchable for easy freight, competitive price, no ground personals needed ; japan xiaosong motor adopted with ff4 remote controller, germany air - use aluminum frame used

    它有飛行平穩，噪音大，廣告面積大，飛行速度慢，易掌握，不用充任何氣體，機翼航空鋁管，全部使用接管方式，運輸極為方便，價格低，不需要地面人員。採用日本小松發動機，日本ff4遙控器，德國蒙皮，航空鋁吊架，風動輪動連體方向。
  14. During last august september and february to april this year, the gfs pilots flew at scheduled times in a twin - engined jetstream j - 41 fixed wing aircraft around lantau island to collect wind and temperature data for the hko

    在去年8 9月及今年2至4月，每星期政府飛行服務隊均安排一架雙引擎捷流式定翼機環繞大嶼山飛行，為天文臺搜集風和溫度數據。
  15. During last august & september and february to april this year, the gfs pilots flew at scheduled times in a twin - engined jetstream j - 41 fixed wing aircraft around lantau island to collect wind and temperature data for the hko. with these data, we can better understand terrain - induced windshear around the airport

    在去年8 、 9月及今年2至4月，每星期政府飛行服務隊均安排一架雙引擎捷流式定翼機環繞大嶼山飛行，為天文臺搜集風和溫度數據。
  16. The mid - sized jet, which will seat up to 330 people, is the first commercial plane whose fuselage and wings are predominantly made of carbon - composite materials rather than aluminum

    787是一種中型噴氣式飛機，最大容量330人，是第一款主要用碳復合材料而非鋁來製造機身和機翼的商用飛機。
  17. Fixed - wing attack types share some similarities with their rotary - wing counterparts, but due to the speed at which the aircraft moves and the differences of fw compared to rw aircraft, they are distinctly different attack types that must be mastered separately

    固定翼飛機的部分攻擊方式與旋翼機相似，但由於其飛行速度與旋翼機不同，另外個別的攻擊方式明顯不同並且高明許多。
  18. 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。
分享友人
分享到 Line

分享到臉書