繞流的 的英文怎麼說

中文拼音 [ràoliúde]
繞流的 英文
circumfluent
  • 繞 : 繞名詞1. [書面語] （彎曲） bend2. （姓氏） a surname
  • 流 : Ⅰ動1 （液體移動; 流動） flow 2 （移動不定） drift; move; wander 3 （流傳; 傳播） spread 4 （向壞...
  • 的 : 4次方是 The fourth power of 2 is direction
  1. 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。
  2. Considering the characters of the viscoidal turbulent flow over high - speed train, the computing model of the outer fiow field for high - speed train has been established based on the incompressible fluid navier - stokes epuation and the turbulent model of ke two equations. the equation set of the flow field problem via finite element methods ( fem ) has been set up

    根據高速列車粘性紊態繞流的特點，在較少簡化的條件下以navier - stokes方程和-兩方程紊流模型為基礎，建立了高速列車外流場的計算模型，在近壁區域採用壁面函數修正紊流模型。
  3. As an example, the implementation of the laplace equation with the gridless method has been presented at first and the resulting large scale matrix equations are solved by gmres algorithm. the numerical simulations of the flows over a cylinder are tested successfully with clouds of different scales, which shows the " cloud " effects on the computational accuracy

    本文先以代表定常不可壓位勢繞流的laplace方程為例，研究了laplace方程的無網格離散形式，並運用gmres高效演算法對其快速求解，數值模擬了典型的圓柱繞流；並通過不同點雲尺度的數值模擬，顯示出點雲尺度對計算精度的影響。
  4. Simulation of flow around cylinder with lattice boltzmann method

    圓柱繞流的lbm模擬
  5. Random vortex method for two - dimensional flow past bluff body

    鈍體繞流的隨機渦方法
  6. Electromagnetic control to cylinder wake

    圓柱繞流的電磁控制
  7. Stability of the crossflow pattern around a slender and influence of disturbance

    細長體截面繞流的穩定性及擾動的影響
  8. Numerical simulation of flows around two bluff bodies in tandem arrangements

    串列鈍體繞流的數值計算
  9. Numerical simulation of flow around blunt bodies using rng k - turbulence model

    湍流模型鈍體繞流的數值模擬
  10. Lattice boltzmann method for oscillatory boundary layer of circular cylinder flow

    方法模擬圓柱繞流的振蕩邊界層
  11. Numerical simulation of viscous flow round a circular cylinder by finite element method

    粘性流體圓柱繞流的有限元模擬
  12. Numerical simulation of turbulent flow around bluff bodies using the rng k - turbulent model

    方法的湍流模型數值模擬鈍體繞流的湍流流動
  13. On the mathematical simulation of non - equilibrium hypersonic flow around the flying vehicle

    關于飛行器高超聲速不平衡氣體繞流的數值模擬
  14. 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顫振問題進行了研究，準確求解跨音速顫振臨界速度，分析機翼和全機的從亞音速到超音速范圍的顫振規律，並研究分析了機翼飛行迎角變化對顫振速度的影響。
  15. A computational method is developed with couples the governing equations of the unsteady flow field and the rigid - body dynamics in six degrees - o f - freedom. 6. facing the complex multi - element and high - lift configuration, a series of methods including multi - zone algorithm and face - to - face technique is developed to lower down the great difficulties of grid generation and finish flow calculation of high - lift system with the dual - time method

    採用基於自適應直角切割網格的分區面搭接方法，結合隱式雙時間推進演算法，實現了三維復雜增升裝置繞流的euler方程數值計算，發展了對存在不連續面的高陞力系統外形進行流場計算的一種方便、實用、高效的三維增升裝置繞流計算方法。
  16. The paper researches the transient time precision and the following problem of the results developing with time for 2 - d high order blocking and matched method, at the same time, anlysing the stability of high order methods including boundary conditions. the results show that the domain decomposition and matched method using high order method can follow the time developing solution of taylor problem well, the computation result of the flow over a single or two tandem arranging circular cylinder agree the experiment and others " results well, moreover, the panting results of lift and drag coefficient are better than others

    本文利用高精度分塊耦合求解方法，對其瞬態時間精度和非定常時間發展解的跟隨性問題進行了研究，同時也對包含邊界條件的線法高精度格式的穩定性也作了分析，研究結果表明高精度的分塊耦合求解方法可以很好地跟隨taylor問題的時間發展解，與單圓柱繞流和雙圓柱繞流的實驗結果比較以及他人結果比較符合很好，對升阻力系數在渦脫落時的脈動問題的結果優於他人結果。
  17. The flow field that results from the interaction of lateral jets injection into supersonic flow over projectile has complicated shocks wave patterns, which include regions of shocks and expand waves, and the lateral jet interaction also effects base flow of projectile

    彈丸側噴流與繞流的相互干擾形成了包含噴口前激波、再附激波以及沿噴流邊界發展的膨脹波等復雜的波系結構，並延伸影響到彈底部流動。
  18. Numerical results show that the present method is effective one for solving the flow around wing with flap deflection

    數值算例表明本方法是求解帶襟翼偏轉的機翼繞流的有效方法。
  19. N - s method for solving the flow around a wing with deflection of flap is presented

    給出了帶襟翼偏轉的三維機翼繞流的一種求解n - s方程的計算方法。
  20. A n - s method for solving the flow around a wing with deflection of flap is presented

    給出了帶襟翼偏轉的三維機翼繞流的一種求解n - s方程的計算方法。
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