撲翼飛機 的英文怎麼說
中文拼音 [pūyìfēijī]
撲翼飛機
英文
flap wing machine-
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。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。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。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。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。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。分享友人