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双语推荐:Navier

对随机Navier-Stokes方程的讨论,通常没有考虑Poisson跳对系统影响.在假设随机的外界环境对系统产生影响的条件下,给出了带Poisson跳的随机Navier-Stokes方程,利用连续鞅的性质,通过公式,Gronwall引理及广义的Gronwall扩展引理讨论了其解的指数稳定性,并给出了指数稳定性的充分条件。
The influence of the P oisson jumps upon the stochastic Navier-Stokes equations has never been consid-ered. This paper discusses the exponential stability of solutions to the stochastic Navier-Stokes equations with Pois-son jumps, on the condition that the system is perturbed by random external environment introducing the definition of solution to the stochastic Navier-Stokes equations and using continuous martingale property, By using Ito^formu-la, Gronwall lemma and extended Gronwall lemma, a sufficient condition of exponential stability is established. This result is an improvement and extension of existing results.

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提出一种基于匹配渐进展开法对Navier-Stokes 方程进行渐进展开求得渐进合成解的方法.在边界层根据边界条件并利用坐标变换放大坐标的方法解出两个同轴旋转圆柱间流体流动Navier-Stokes方程的内解,并在Navier-Stokes方程的外解已经解出的基础上根据内、外解的匹配原则对内、外解进行匹配,从而解出具有二阶有效、简洁的渐进合成解.通过举例证明,该合成解准确性好并且与基本流接近程度很好.
@@@@Based on the matching asymptotic expansion method , the authors develop a new method to solute the composite solution for the Navier -Stokes equation.The interior solution of Navier -Stokes equation is solved by using the boundary conditions and the way of coordinate transformation at boundary region .In accordance to the matching of outer solution and interior solution , the second, effective and concise gradual composite solution is solved and this method is on the basis of the finished outer solution .For example, the accuracy and the degree of closeness to the basic flow is very well ..

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Temam提出求解稳态Navier-Stokes方程的Uzawa算法并且证明了算法的收敛性.然而,至今没有算法的收敛率分析.本文证明该算法是以几何级数收敛的.
Temam proposed an Uzawa algorithm for solving steady incompressible Navier-Stokes equations and proved its convergence. However,the convergence rate analysis remains open until now. We prove in this paper that this method converges geometrically.

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数值求解非定常不可压缩Navier-Stokes方程的难点之一在于强烈的非线性容易引发非物理震荡,本文结合可以有效减弱此种震荡的特征线离散方法,基于局部Gauss积分之差的稳定化格式,采用最低等阶非协调混合有限元对NCP1-P1,构造出求解非定常不可压缩Navier-Stokes方程的特征稳定化非协调混合有限元方法。证明了该方法的全离散格式是无条件稳定的,并给出逼近解的相应误差估计。
One of the difficulties for numerical simulation of the unsteady Navier-Stokes equa-tions is the nonlinearity, when characteristic discretization can effectively weaken the non-physical concussion caused by nonlinear form. Based on the local Gauss quadrature, this paper proposes a characteristic stabilized nonconforming finite ele-ment method to solve the unsteady incompressible Navier-Stokes equations, where the characteristic method and lowest equal-order nonconforming pair NCP1-P1 are employed. We obtain the unconditional stability of its full discrete format and the corresponding error analysis of the approximate solutions.

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讨论了随机 Navier-Stokes方程的近似最优控制问题。利用 Ito^公式,Burkholder-Davis-Gundy不等式,伴随方程以及极大值原理,证明了近似最优控制存在的充分条件。
In the paper,the near-optimal control problems of stochastic Navier-Stokes equation are discussed.The sufficient conditions for the near-optimal control are proved by Ito^′s formula,Burkholder-Davis-Gundy inequation,adjoint equation and maximum principle.

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本文研究了L′evy过程驱动的随机二维Navier-Stokes方程弱解的指数性态.给出了不同条件下解的长时间形态,获得了一些特殊情形下解的样本轨道的指数稳定性.
In this paper, some results on the pathwise exponential stability are established for the weak solutions of stochastic 2D Navier-Stokes equation driven by L′evy noise. Also, some results and comments concerning the stabilizability and stabilization of these equations are stated.

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基于Hermite多项式的C1型单元构造复杂,限制了最小二乘有限元法的应用.引入高阶光滑的非均匀有理B样条作为基函数简化C1型单元构造,提出求解黏性不可压流动Navier-Stokes方程的最小二乘等几何方法.用Newton法或Picard法对Navier-Stokes方程线性化,用线性化偏微分方程的余量定义最小二乘泛函,导出最小二乘变分方程,用NURBS构造高阶光滑的有限维空间来近似速度场和压力场.计算表明:本文方法计算的二维顶盖驱动流数值解能准确描述流动状况,计算的二维通道内圆柱绕流全局质量损失由最小二乘有限元法的6%降为0.018%,该方法可用于Navier-Stokes方程的求解,并且具有较好的质量守恒性.
With high order smooth non?uniform rational B?splines ( NURBS) as basis function to simplify C1 element construction, least squares isogeometric analysis is proposed for viscous incompressible Navier?Stokes equations. Governing equations are linearized by Picard or Newton method. Variational equation is derived from least squares functional defined by residuals of linearized equations. High order smooth finite dimensional spaces for velocity and pressure approximation are constructed by NURBS. Two benchmark flow problems were solved. Accurate numerical results were obtained for 2?dimensional lid driven flows. Global mass loss in flow past a cylinder in a channel decreased from 6% in classical least squares finite element method to 0?018%. It shows that the method is applicable to Navier?Stokes equations. It is better in mass conservation than least squares finite element method.
In this article, we prove the local existence and uniqueness of the classical solution to the Cauchy problem of the 3-D compressible Navier-Stokes equations with large initial data and vacuum, if the shear viscosity μ is a positive constant and the bulk viscosity λ(ρ) = ρβwith β≥ 0. Note that the initial data can be arbitrarily large to contain vacuum states.
In this article, we prove the local existence and uniqueness of the classical solution to the Cauchy problem of the 3-D compressible Navier-Stokes equations with large initial data and vacuum, if the shear viscosity μ is a positive constant and the bulk viscosity λ(ρ)=ρβwith β≥0. Note that the initial data can be arbitrarily large to contain vacuum states.
微型扑翼体积小、重量轻,其柔性变形对气动特性有显著的影响。通过求解雷诺平均 N-S 方程(Reynolds-Averaged Navier-Stokes,RANS)和结构动力学方程,对微型柔性扑翼飞行器的气动结构耦合特性进行了数值模拟研究。针对微型扑翼的大幅运动,发展了适用于扑翼的气动结构耦合数值计算方法,研究了微型扑翼的气动结构耦合特性。通过求解雷诺平均 Navier-Stokes(RANS)方程得到微型扑翼的非定常气动特性;利用哈密顿原理(Hamilton Principle)推导了扑翼的结构动力学方程,采用结构有限元方法对该动力学方程进行离散并求解,得到扑翼的动态结构特性;采用松耦合方法进行迭代。计算结果与风洞实验结果相比吻合良好,验证了所发展方法的有效性。在此基础上研究了惯性力和关键运动参数对柔性扑翼气动及结构特性的影响规律,有助于比较详细、全面地了解微型扑翼的气动机理,为柔性扑翼的设计提供了参考依据。
Due to the small size and light weight,flexible deformation plays an important part in flapping wing aerodynamics.the aero-elastic performances of Flapping-wing Micro Air Vehicle (FMAV)are researched by solving the Reynolds-Averaged Navier-Stokes (RANS ) equations and structural dynamic equations.An aerodynamic-structural coupling computational framework is developed,which is able to simulate aerodynamic-structural coupling characteristics of flexible flapping wings.The flapping wing′s unsteady aerodynamic characteristics is obtained by solving Reynolds Average Navier-Stokes (RANS)equations.Structural dynamic equations capable of describing the flapping wing′s movement are derived by using Hamilton principle,then discreted through finite element method and solved by Newmark solution to get structural characteristics.Loose coupling method is used.On the basis of the above work,CFD/CSD (Computational Fluid Dynamics/Computational Structural Dynamics)grid data exchange method,
为了研究边界滑移对上游泵送机械密封性能的影响,建立液膜三维几何模型和计算模型,基于 Navier 线性滑移模型对液膜壁面边界条件进行修正,采用商用软件 Fluent 的 SIMPLEC 算法及层流模型求解三维 Navier -Stokes 方程,并分析相对滑移量对液膜静压分布、开启力、摩擦扭矩、泄漏量的影响规律。结果表明:相对于边界滑移发生的位置,滑移速度的大小对密封性能的影响更大;当相对滑移量较小时,存在边界滑移与无滑移的模拟结果无明显区别,能很好地解释宏观无滑移边界假设的应用,当相对滑移量较大时液膜动压效应随滑移的增加而减弱,开启力、摩擦扭矩、泄漏量都随边界滑移的增加而减小;相对于开启力的降低,边界滑移的减阻和降低泄漏的效果更为明显;当开启力较小,应避免边界滑移发生;当开启力足够大时,加工成超疏水表面形成边界滑移,可极大地减少摩擦扭矩,降低能耗。
To study effects of boundary slip on performance of upstream pumping mechanical seal,the geometric and computational models of fluid film are built.The Navier -Stokes equations of the fluid film flow are solved in Fluent by employing SIMPLEC algorithm and finite volume method.The boun-dary conditions are modified with the Navier linear slip model and the effects of boundary slip on the film pressure distribution,opening force,friction torque and fluid leakage are analyzed.The results show that the slip velocity has a greater influence than the location of slip occurrence.When the slip velocity is tinier,the results of simulation are almost the same as the data without slip,indicating the non-slip assumption for macro flow of a fluid is reasonable.However,when the slip is larger,the dy-namic effect of fluid film is weakened and the opening force,friction torque and fluid leakage are de-creased with the increasing slip velocity.Additionally,the reduction in both friction torque

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