flapping wing 中文意思是什麼

flapping wing 解釋
撲翼的
  • flapping : 揮拍的
  • wing : n 1 翼，翅膀；鳥；鳥群；飛行，飛翔。2 （飛機）機翼；翼狀物；（汽車的）擋泥板；〈詩常 pl 〉船帆。3...
  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. 2. the 3 - d unsteady euler equations are derived. and the computational program based on these equations is developed to adapt for the calculations of flapping wing

    2 、推導了非定常情況下的三維歐拉方程，發展了三維非定常歐拉方程計算程序，使之適應于撲動翼計算的需要。
  5. Flexibility of flapping wing and its effect on aerodynamic characteristic

    撲翼柔性及其對氣動特性的影響
  6. It is concluded that all of the tested bionic wings can generate lift force, however the flexible wing has best kinetic and aerodynamic performance among them, as well as flapping frequency and amplitude are the main factor of effecting on lift force generation

    實驗結果表明，研製的翅型都能產生一定的升力，其中柔性翅具有較好的運動性能和氣動性能，並且拍動頻率和拍動幅度對升力有較大影響。
  7. 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。
  8. 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。
  9. 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。
  10. 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。
  11. 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。
  12. 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。
  13. Aimed at the mechnical flapping wing system of the bionicflying micro - robot including the micro - actuators, the bionic wing, the locomotion system, and the energy source, the scaling effect is analyzed

    針對微型仿生撲冀飛行器的機械撲冀系統，包括微驅動器、仿生翅、運動系統和動力源等，本文進行了尺度效應分析。
  14. 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。
  15. Takuma sato made a superb start to run 14th at the end of the opening lap, but later suffered a flapping engine cover wing at one stage before retiring with a hydraulic problem

    佐藤琢磨完成了一個超級出色的發車，在第一圈之後跑在了第十四位，但之後在他因為液壓問題退賽之前，他因為顫動的引擎蓋翼掉到了後面。
  16. Results show that the bionic flying can be more easily realized when the scaling sizes are decreased, thus making high flapping frequency motion by the resonance, and meeting the power needs of the flapping wing for the electrostatic, the electromagnetic and piezoelectric actuators

    分析結果表明，當尺寸減小時，仿生飛行更容易實現：通過共振能實現高頻運動，微靜電、電磁和壓電驅動器都能滿足撲翼系統功率需求。
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