迎风

yíng fēng
  • windward;against the wind;facing the wind;down the wind
迎风迎风
迎风 [yíng fēng]
  • (1) [facing the wind]∶面对着风吹的方向

  • 迎风飞翔

  • (2) [down the wind]∶随着风吹去的方向

  • 彩旗迎风招展

迎风[yíng fēng]
  1. 她很讨厌风天,因为迎风时她呼吸会很困难。转舵背[迎]风!

    She hates the wind very much because she cannot breathe easily when facing the wind .

  2. 坐在这里正迎风,特别凉爽。

    It 's nice and cool to sit here against the wind .

  3. 红旗迎风飘扬。

    The red flags are waving in the breeze .

  4. 船帆迎风鼓起。

    The sails swelled out in the wind .

  5. 柳条迎风摆动。

    The willows swayed in the breeze .

  6. 迎风使舵!

    Helm aweather !

  7. 细柔的柳枝迎风摇曳。

    The slender willow branches were swaying gently in the breeze .

  8. 柳枝迎风摇曳,婀娜多姿。

    Willow branches are fluttering ( or swaying ) gracefully in the breeze .

  9. 彩旗迎风飘扬。

    The colored flags flow in the wind .

  10. 五彩缤纷的旗帜迎风飘扬。

    Colourful flags are fluttering in the breeze .

  11. 通过一阶迎风格式及QUICK格式,求解出该模型的数值解。

    The numerical simulation of this model was analyzed through first-order upwind difference scheme and QUICK scheme .

  12. 组合的LU分解迎风方法的多重网格收敛

    Multigrid convergence of a combined LU-factored upstream method

  13. 每一个人都知道这些人隶属于LeT。很快地,他们画有黑与白与交叉双剑的旗帜在山谷中迎风飘扬。

    Everyone knew these men belonged to LeT , and soon their black and white banners with crossed swords were flying everywhere in the mountains and valleys .

  14. 控制容积界面上的函数值采用了具有迎风倾向的QUICK格式。

    The functional value on the interface of the control volume is calculated using the QUICK scheme with upwind style . 3 .

  15. 模拟时采用标准k-ε模型方程,压力与速度的耦合采用SIMPLE算法,动量、湍动能、耗散率均采用二阶迎风格式离散。

    The equation is K-E model , the coupling of velocity and pressure used SIMPLE method . Momentum turbulence kinetic energy and turbulence dissipation rate are second order upwind .

  16. 运用迎风格式和Euler向前差分格式进行求解。

    An upwind scheme and forward-Euler difference method are considered for the approximation .

  17. 数值求解Navier-Stokes方程的迎风紧致差分格式

    A high order accurate upwind compact scheme for solving Navier-Stokes equations

  18. 对流-扩散问题的Galerkin部分迎风有限元方法

    Galerkin partial upwind finite element method for the convection-diffusion equations

  19. 粘性流体大幅晃动的ALE迎风有限元方法

    ALE Upwind Finite Element Methods for Viscous Flow with Large-Amplitude Sloshing

  20. 定常不可压Navier-Stokes方程迎风格式

    An Upwind Scheme for the Incompressible Navier-Stokes Equations

  21. 解Burgers方程的部分迎风有限元法与离散极值原理

    On partial upwind finite element method and discrete maximum principle for Burgers equations

  22. 数值计算采用了涡团耗散湍流燃烧模型、可实现k-ε湍流模型和离散坐标系辐射模型,SIMPLE压力速度耦合算法以及二阶精度迎风插值格式。

    The eddy-dissipation turbulent combustion model , realizable k - ε turbulent model , discrete ordinates radiation model , SIMPLE pressure-velocity coupling method and second-order upwind discretization scheme were adopted in the numerical simulation .

  23. 提出了一种交错的有限体积迎风格式算法,用以联合求解NS方程与Kω湍流模型方程。

    A staggered finite volume upwind algorithm for solving the compressible NavierStokes equations and the K ω turbulence model equations has been developed .

  24. 通过Fourier分析法评估了这些迎风偏斜格式的耗散误差与频散误差。

    The dispersion and dissipation errors of upwind-biased finite difference schemes are assessed and compared by means of a Fourier analysis of the difference schemes .

  25. 迎风型TVD格式在高速进气道粘性流动模拟中的应用

    Application of upwind TVD scheme to numerical simulation of supersonic inlet

  26. 迎风TVD格式在粘性流计算中的应用研究与改进

    The study and modification of upwind TVD scheme for computing viscous flows

  27. 二阶迎风TVD数值格式在非平衡高超声速钝体绕流中的应用

    Applications of a second-order upwind TVD scheme to nonequilibrium hypersonic flows around blunt-body

  28. 一阶迎风和二阶ENOLocalLax-Friedrich格式的修正系数研究

    On modifying coefficients of first-order upwind scheme and second-order eno local lax-friedrich scheme

  29. 破片迎风面积测量控制系统,整个控制系统由面阵CCD相机、力矩电机,编码器、单片机主控单元等组成。

    The controlling system of measuring fragment frontal area consists of a CCD camera , a absolutely moment motor , photoelectricity coder and a computer control cell .

  30. 利用自适应Delaunay三角剖分并结合胞格中心迎风算法,分析非粘滞高速可压缩流体问题。

    Adaptive Delaunay triangulation is combined with the cell-centered upwinding algorithm to analyze inviscid high-speed compressible flow problems .