1) primitive-variable N-S equation
原参数N-S方程
2) Navier-Stokes simulation
N-S方程数值解
3) N-S equations
N-S方程
1.
Solving 2-D unsteady incompressible N-S equations with compact finite difference scheme;
紧致差分格式求解二维非稳态不可压N-S方程
2.
A Method of using chimera grid and N-S equations for calculation of the flow around multi-element airfoils;
N-S方程多段翼型绕流计算的嵌套网格方法
3.
Bi-point/bi-objective optimization design of ailfoil using N-S equations;
基于N-S方程的翼型双设计点双目标优化设计
4) navier-stokes equations
N-S方程
1.
Computation of flows around projectile bodies with base jet using finite-volume method of Navier-Stokes equations;
用N-S方程有限体积法计算弹体绕流/底喷流
2.
Solution method for Navier-Stokes equations using highly irregular control volumes;
用任意不规则网格求解N-S方程
3.
A time-derivative preconditioning algorithm is implemented to solve three-dimensional steady/unsteady Navier-Stokes equations on hybrid grids.
运用时间导数预处理法在混合网格上求解三维定常/非定常N-S方程。
5) Navier-Stokes equation
N-S方程
1.
Since the limitation of Reynolds equation in lubrication,one way of computational fluid dynamics(CFD) approach which based on Navier-Stokes equation was advanced to solve lubrication questions.
在分析雷诺方程求解流体润滑问题上的不足与局限性的基础上,给出了基于N-S方程的计算流体力学(CFD)求解流体润滑问题的方法。
2.
Three-dimensional Navier-Stokes equation is used to calculate the centrifugal compressor perfo.
使用三维N-S方程对所设计的离心压气机在设计点的性能进行了计算,计算结果表明所设计的离心压气机基本能够满足设计要求。
3.
The 3-D inner flow field of sidewall compression hypersonic inlet and the isolator is numerically studied by solving the 3-D Navier-Stokes equation.
用 N-S方程和 RNG k-ε紊流模型计算了 RBCC用侧压式高超音速进气道三维内流场 ,重点分析了马赫数对流场的影响。
补充资料：参数方程
参数方程
parametric equation
参数方程「碘门旅州c闰.d佣;naP明e甲明ec劝e冲a-朋eHHe〕空间中点集的 集合的点或它们的坐标的一种具体表述，它由某些称为参数(paJ旧n犯te侣)的变量的函数之值所给出. n维向量空间R”中直线的参数表示有如下形式: x=x(0，+。r，x(“)，a e Rn，一的
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参考词条