wing theory 中文意思是什麼

wing theory 解釋
機翼理論
  • 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...
  • theory : n. 1. 理論，學理，原理。2. 學說，論說 （opp. hypothesis）。3. 推測，揣度。4. 〈口語〉見解，意見。
  1. The new technique allows first order shear deformation plate theory ( fsdpt ) or classical plate theory ( cpt ) to be used for modeling built - up wing structures, sandwich wing structures or the wing structures which the volume between upper and lower skin is empty or solid with a ' general planform

    根據翼面的幾何和結構特點，新技術能夠自主選擇經典板理論（ classicalplatetheory ，簡稱cpt ）或第一階剪切變形板理論（ firstordersheardeformationplatetheory ，簡稱fsdpt ） ，具有模擬空心、實心、夾層和組合等形式的翼面結構及三維建模的能力。
  2. Rethinking the theory of left - wing drama popularization

    左翼戲劇大眾化理論的再思考
  3. The potential flow theory is then applied to the overlap of the slipstream and the flow over the wing

    用位流理論來處理螺旋槳滑流與機翼繞流的迭加。
  4. According to biologic viewpoint, all volant animal, its condition is posture necessarily lightsome, wing is very wide ; and bumblebee this kind of biology however as it happens follows this theory to do exactly the opposite : the body of bumblebee is very heavy, and wing is however very smallish

    根據生物學的觀點，所有會飛的動物，其條件必然是體態輕盈、翅膀十分寬大；而大黃蜂這種生物卻正好跟這個理論反其道而行之：大黃蜂的身軀十分粗笨，而翅膀卻是十分的短小。
  5. This paper deals with loop subdivision and its extension, the main work is as follows : ( 1 ) loop subdivision scheme and its extension are implemented via the wing - edged structure, then subdivision theory is introduced together with some important conclusions in exact computation

    本文主要對loop細分曲面及其擴展進行了研究，內容包括： （ 1 ）首先採用翼邊結構對loop細分演算法及其擴展進行了實現，然後對細分曲線曲面理論和精確計算方面的重要結論作了研究。
  6. In order to set up the dynamic model of swimming micro robot, this dissertation builds up the statics model and analyses the micro motion amplifying performance of micro robot mechanism, builds up the vibration model of micro robot and analyses the vibrating performance without and with damp, researches the propelling force of driven wing and the resistance of micro robot in liquid based on the theory of flat board resisting stream, builds up the dynamic model of swimming micro robot for the first time in nation and analyses its swimming performance which is influenced by driving signal frequency, amplifying performance of main machanism, area of driven wing, character of fluid and so on. this dissertation manufactures the micro robot and sets up the experimental environment and tests the amplifying effect and the vibrating performance

    本文建立了主體機構靜力學模型，研究了主體機構的結構參數對微位移放大性能的影響；建立了主體機構振動模型，研究了主體機構在無液體阻尼和有液體阻尼情況下的振動特性；根據流體力學平板繞流理論，研究了驅動翼產生的推進力和微機器人在流體中受到的阻力；在此基礎上國內首次建立了泳動微機器人的動力學模型，並對模型進行了深入的研究，詳細闡明了驅動信號頻率、主體機構放大性能、主體機構振動特性、驅動翼面積、液體性質等因素對微機器人泳動特性的影響。
  7. Based on the potential theory, linear and fully nonlinear aerodynamic forces and motions of a wing flying above sea - waves are studied numerically. and the effects of the characteristic parameters of wing and sea waves on the aerodynamic forces are acting on the wig are analyzed systematically in this thesis

    本文基於勢流理論計算研究了二維和三維機翼在風浪擾動中的線性和全非線性氣動力及其運動響應，全面分析了機翼和波浪的特徵參數對氣動力的影響，得出了很多有意義的結果。
  8. Using multidisciplinary collaboration simulation, applying aeroelastic theory and method, structural modeling with fem was set up, structural dynamics and vibration mode were analyzed, and then problem of gust load alleviation for a large flexible wing was discussed

    摘要利用多領域協同模擬技術，應用氣動彈性分析理論和方法，對柔性機冀進行結構有限元建模、動力學特性分析、固有振動分析，並針對垂直陣風載荷減緩進行討論。
  9. We generated its grid surface on the fuselage or missile body according to the geometry projection relation between aerodynamic components and the bilinear interpolation approach. finally, we successfully developed a new algebra grid generation technique in virtue of the improved four - boundary interpolation. in this thesis, we put emphasis on the researches of aerodynamic inverse design and drag reduction questions for airfoil and wing using euler equations and control theory proposed by jameson

    （ 2 ）進行了應用控制理論和二維歐拉方程的翼型氣動反設計，以及有升力約束情形下翼型跨音速減阻問題研究，分別推導了相應的共軛方程及邊界條件的數學形式，並給出了相應的梯度求解公式形式，研究發展了共軛方程及梯度的數值求解方法，成功進行了多個翼型的反設計和減阻問題研究。
  10. According to the theory of boundary layer and the important of boundary - layer separation point detection of delta wing, the measuring principle and structure scheme of various system alternatives based on mems technology have been discussed, selecting the prototype of better workability. base on the master piece model of micro shear stress sensor

    首先，結合空氣動力學的邊界層原理，針對三角翼邊界層分離點檢測在實現主動氣動控制方面的重要性，討論了光學式、電容式和熱敏式微型剪應力傳感器的測量原理和結構方案，選取適合加工條件的微型剪應力傳感器樣件。
  11. 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。
  12. According to the theory of boundary layer control and aerodynamics of delta wing at medium attack angle, the generation mechanisms of rolling, pitching, yawing moments, which are produced by coupling between the microactuator array and boundary layer near the leading edge, have been discussed

    首先，結合空氣動力學的邊界層控制原理以及三角翼在中等攻角條件下的氣動特徵，詳細討論了微致動器陣列通過與前緣邊界層的耦合產生三角翼翻滾、俯仰和偏航等力矩的機理。
  13. Wing counters that those who use language with ease, as tito does, indeed perform well on tests of the theory of mind

    溫恩則反駁說，像第托這種能輕易使用語言的患者，確實在心靈理論的測驗當中表現良好。
  14. It has been said in chaos theory that something as small as the flutter of a butterfly ' s wing can ultimately cause a typhoon halfway around the world. if global climate could be influenced by a butterfly, what will a mosquito do the destiny of a human being

    根據混沌理論，一尾蝴蝶扇動翅膀能夠掀起世界另一端的風暴，如果一尾蝴蝶的力量便足以牽動全球氣候，那麼一隻蚊子是否也可能改變一個人的命運？
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