顫振運動 的英文怎麼說

中文拼音 [zhànzhènyùndòng]
顫振運動 英文
zitterbewegung
  • : 顫動詞(發抖) shiver; shudder; tremble
  • : 動詞1. (搖動; 揮動) shake; flap; wield 2. (奮起) brace up; rise with force and spirit
  • : Ⅰ動詞1 (物體位置不斷變化) move; revolve 2 (搬運; 運輸) carry; transport 3 (運用) use; wield...
  • 運動 : 運動[舊時用語] arrange things or get things done through pull
  1. On the bases of carrying out idle operation, cutting and modal experiment of certain numerical controlled lathe, it is determined that weak dynamic stiffness in the spindle component of machine tool is the reason in the respect of structure for causing cutting vibration of machine tools

    摘要在對某型數控車床進行空轉、切削及模態試驗的基礎上,確定了機床主軸部件剛度薄弱是引起機床切削的結構方面的原因。
  2. Finally, the 2d unsteady navier - stokes flow solver is coupled with two - degree - of - freedom flutter motion equation in time domain to investigate the flutter characteristics of several supercritical airfoils

    最後,本文將二維非定常nayier - stokes方程解算器與顫振運動方程耦合,研究了超臨界翼型的跨音速特性。
  3. Then the steady and unsteady subsonic, transonic and supersonic viscous flows around airfoil and some aircraft are numerically simulated. the 3 - dimensional unsteady navier - stokes equations are solved using the implicit lu - nnd algorithm, with baldwin - lomax turbulent model. on the basis of simulating unsteady viscous flow, coupling the structure dynamics equations, the problems of static aeroelasticity and flutter are investigated for wings and elevator

    在模擬非定常粘性繞流的基礎上,與顫振運動方程相耦合,分別對機翼和全機流固耦合現象中問題進行了研究,準確求解跨音速臨界速度,分析機翼和全機的從亞音速到超音速范圍的規律,並研究分析了機翼飛行迎角變化對速度的影響。
  4. Apart from the mathematical properties of the dirac operator we investigate the behavior of observables such as position, velocity, momentum, describe the zitterbewegung, and formulate the localization problem

    除了狄拉克算元的數學工具之外,我們研究諸如位置,速度,量等看得見的客觀屬性,描述了,並闡述一些局部問題。
  5. Flutter is the most important instable problem and it restricts the flight envelope and performance of a vehicle. aeroservoelasticity, including active flutter suppression technology, is a multidisciplinary optimization technology that studies the interaction of flexible structure, unsteady aerodynamics and flight control system

    以主抑制系統設計為代表的氣伺服彈性力學( ase )是一門涉及柔性結構、飛行器引起的定常和非定常氣力以及飛行控制系統相互作用的多學科技術。
  6. In addition, aerodynamic stiffness and aerodynamic damping on the system are already obtained in the condition of fluid - structure interaction. it is known that aerodynamic loads are associated with blade vibration. the systematic eigenvalues are used to judge whether the flutter occurs so as to find the stable operating range of a wind turbine

    本文把風力機葉片簡化為懸臂梁,對梁截面的二維葉型建模,完整推導了二維葉型的線性微分方程和流構耦合條件下系統的氣剛度和氣阻尼,此時氣載荷與結構的位移矢量以及速度矢量是相互耦合的,再利用系統的特徵值來判斷葉片是否發生,從而獲得風機的穩定工作范圍。
  7. As a special form of vibration, flutter is a major feature closed with the run environment and safety of aircraft, which is an important project of human - machine - environment engineering

    作為一種特殊的形式,與飛行器的行環境和安全性密切相關,是人機與環境學科的一個重要研究課題。
  8. One is null oscillation occurred in the ehs valve, the second is the failure in the torque motor circuit, and the third is the load disturbance in the actuator

    然後對系統中其他幾種故障作了分析,包括伺服閥中位故障;線圈故障;液壓缸慣性變化故障。
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