撲翼的 的英文怎麼說

中文拼音 [pūyìde]
撲翼的 英文
flapping wing
  • 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...
  • 的 : 4次方是 The fourth power of 2 is direction
  1. Status and prospects of driving mode about the wing for the bionics flapping aerocraft

    仿生撲翼飛行器翅翼驅動方式的研究現狀及展望
  2. The main aspects of this dissertation are as follows : 1. employing the moving grid technique, a 3 - d moving grid based on the transfinite interpolation is developed. this grid has better adaptation than the deforming grid for flapping wing

    本文的主要工作表現在以下幾個方面： 1 、引入運動網格技術，發展了一套基於廣義無限插值理論的適合撲翼計算的三維運動網格，提高了網格對撲動機翼的適應性。
  3. Attitude tracking control for flapping wing micro aerial vehicle based on feedback compensation

    基於反饋補償的撲翼微型飛行器姿態跟蹤控制
  4. Emre links well with pasquale on the left then crosses into the middle. the ball deflects off colucci, forcing pagliuca into a near - post save

    在左翼埃姆雷與小帕巧妙配合后傳中，球被科盧奇碰了一下改變方向，帕柳卡做出了一次近門柱的撲救。
  5. Recoba plays his right - wing corner to the far post. . calderoni is beaten and cruz heads wide to waste another chance

    雷科巴的左翼角球開遠門柱，卡爾德羅尼撲了一下，克魯茲頭球攻門偏出，浪費了又一次機會。
  6. Aerospace series. rowings. measurement of the equitension of the base strands

    航空航天系列.撲翼機.底板絞線的等拉伸力的測量
  7. Flexibility of flapping wing and its effect on aerodynamic characteristic

    撲翼柔性及其對氣動特性的影響
  8. The development and test on wing type of a bionic flying micro - robot

    仿生撲翼飛行機器人翅型的研製與實驗研究
  9. The bionic flying micro - robot is a complicated intelligent robot, i. e. and a micro aerial vehicle

    摘要微型仿生撲翼飛行器是一種新概念的微型飛行器。
  10. The modeling and analysis method, as well as the conclusions are helpful to the design, fabrication and application of fmav

    文中的建模、分析方法及所得結論為微撲翼飛行器機翼的設計、製作和應用提供了一定的理論依據。
  11. Applying this dissertation, the aerodynamic characteristics of flapping wing can be calculated, the effects of every factor can be analyzed and some qualitative instructions can be given

    運用本文可以計算撲翼的氣動特性及分析各參數對撲翼氣動特性的影響，進而指導撲動翼微型飛機的初期設計。
  12. 5. effects of unsteady flows on the aerodynamic characteristics are also analyzed. the results of this dissertation are useful for the further investigations of three - dimensional flapping wing

    對于非定常不可壓流動，分析了運動參數對翼型氣動特性的影響，為進一步研究繞三維撲翼的非定常流動打下基礎。
  13. The design and fabrication of high efficient biomimetic wings with good dynamic characteristics are the keys of fmav. meanwhile, it ’ s also a very challenging research topic at present

    設計和製造具有良好動力學特性的高效仿生翼，是仿生微撲翼飛行器研究中的一個關鍵環節，同時也是目前非常富有挑戰性的研究難題。
  14. 3. the effects of every flapping control parameters on the aerodynamic characteristics of flapping wing are investigated. its results lay a foundation for the further investigations of flapping wing micro air vehicles

    3 、研究了運動各參數對撲翼的氣動特性的影響，為撲翼微型飛機的進一步研究設計打下了基礎。
  15. Combined with blade element theory, the results can be used to evaluate aerodynamic characteristics of flapping wings, which are helpful for the initial design of micro rotary and flapping wing

    運用本文方法分析了各參數對翼型氣動特性的影響，進一步結合葉素理論還可以估算撲翼的氣動特性，進而指導微旋翼或撲翼微型飛行器的初期設計。
  16. In this thesis, finite volume method and dual - time stepping method are employed to solve the 3 - d unsteady euler equations. the unsteady flow field around a finite - span flapping wing is simulated. the lift and thrust of the flapping wing for different cases are calculated

    本文運用有限體積法結合雙時間推進技術求解三維非定常歐拉方程，模擬了有限翼展機翼在同時具有上下拍動和俯仰運動狀態下的非定常流場，計算了不同狀態下撲翼的升力及推力，分析了各個影響因素對撲翼氣動特性的影響。
  17. The flapping wing system of a bionic flying micro - robot based on insects and birds aggregates the lift, hovering and push functions, its kinematics and aerodynamics are different from that of fixed wing and rotational wing, and so bionic flying micro - robot must be studied from bionics initially

    摘要模仿昆蟲和小鳥飛行的撲翼飛行機器人將舉升、懸停和推進功能集於一個撲翼系統，與固定翼和旋翼完全不同，因此研究只能從生物仿生開始。
  18. Then, the modal analysis of two differently typical biomimetic wings are conducted and their modal parameters as nature frequency and vibration modes are obtained. as a result, the plane - structure wings with shell elements for fmav is not ideal comparing with the truss - structure wings composed by shell and pipe elements

    利用ansys軟體對兩種結構類型的仿生翼進行模態分析，得到其低階固有頻率及振型等模態參數，並由結果指出純殼單元平板結構作為微撲翼飛行器的機翼不夠理想，而採用梁單元和殼單元的復合結構是設計微撲翼飛行器機翼的一個方向。
  19. Flapping - wing micro air vehicles ( fmav ) are new conceptual air vehicles. they surpass the research fields of traditional airplane design and aerodynamics in relation to application technologies, and initiate the applications of mems technologies to aviation fields

    微撲翼飛行器是一種模仿鳥類或昆蟲飛行的新概念飛行器，在應用技術上它超出了傳統的飛機設計和氣動力的研究范疇，同時開創了微機電系統技術（ mems ）在航空領域的應用。
  20. Grid generation is a pivotal technology of cfd ( computational fluid dynamics ). follow the complication of problem in cfd field, the grid generation technology has developed in two ways : in the first place, it improved grid generation method to adopt the increasingly complicated figuration ; on the other hand, it developed new methods to deal with the problem including fluctuant surface, such as multi - body separation problem etc. among this ways, the overlap grid technology is a vive research aspect

    網格技術是cfd （ computationalfluiddynamics ）領域中的關鍵技術。隨著cfd涉及問題的復雜化，網格技術在兩個方向上逐步發展:一方面針對不斷復雜的外形處理需求改進網格方法，從而能夠模擬復雜飛行器及其各個氣動部件的細節;另一方面發展適應撲翼、多體分離等變幾何外形問題的網格方法，使得cfd的工程應用領域不斷拓寬。這其中，重疊網格方法是一個較有活力的研究方向。
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