euler equation造句
例句与造句
- The differentiator series solution to euler equation
欧拉方程的微分算子级数解法 - The numerical solution of euler equations is provided as flowsolver
翼型的流场解由欧拉方程的数值解提供。 - Euler equations of hydrokinetics
欧拉铃运动方程 - Euler equation for turbomachine
欧拉涡轮机方程 - Numerical methods of multicomponent flowsof non - conservative euler equations
多介质流体非守恒律欧拉方程组的数值计算方法 - It's difficult to find euler equation in a sentence. 用euler equation造句挺难的
- Solving method for inverse problem of unsteady aerodynamic design of 2 - d oscillating airfoil based on euler equations
二维机翼非定常气动反命题的欧拉解法 - Then , similar to the 3 - d euler equations , the blow - up criterion of the classical solution for the 3 - d boussinesq equations without viscosity term is given
然后，与三维euler方程类似，本文给出了三维无粘boussinesq方程组古典解的爆破准则。 - In chapter one , we consider the characteristics - mixed finite element numerical simulation for the euler equation for an incompressible fluid with zero viscosity in two dimensions
本文讨论了两类发展方程二维不可压无粘流问题和线性积分微分方程的数值模拟。 - Jameson finite volume scheme and four - stage rung - kutta time - stepping method are employed in the process of the zonal parallel computation of euler equations
在euler方程的分区并行计算过程中，本文采用了jameson有限体积法和四步runge - kutta显示时间推进格式。 - With which this paper develops a plat to get 3d geometries " euler equation flow solution using jameson ' s finite volume method ( fvm ) techniques
本文通过对三维直角切割网格生成方法的研究，应用jameson的有限体积法建立了一个基于直角切割网格技术的流场计算软件。 - 2 . the 3 - d unsteady euler equations are derived . and the computational program based on these equations is developed to adapt for the calculations of flapping wing
2 、推导了非定常情况下的三维欧拉方程，发展了三维非定常欧拉方程计算程序，使之适应于扑动翼计算的需要。 - A muscl type cell - centered finite - volume scheme is presented for solving the 3 - d time - dependent euler equations cast in an arbitrary lagrangian - eulerian ( ale ) framework
构造了一种muscl ( monotonicupwindschemesforconservationlaws )类型有限体积格心( cellcentered )格式对方程进行离散。 - The three - dimensional ( 3d ) euler equations are applied to the study of numerical simulation of chemical non - equilibrium oblique detonation wave standing on an accelerating projectile with attack angle
摘要采用三维非定常化学反应控制方程组对驻定在带攻角高速飞行弹丸上的斜爆轰波流场进行了数值模拟。 - First , hydrogen - air scramjet combustor is numerically simulated and analyzed by solving the general one - dimensional unsteady euler equation . second , compressible , reacting , turbulent flow solutions are obtained
通过求解广义一维非定常euler方程，数值模拟了氢燃料的燃烧室，并和实验结果进行了比较和分析。 - With introduction of pseudo compressibility , two - dimensional euler equations are derived . referring to compressible method , central finite volume scheme is employed to develop a computational code
参照可压缩流动计算的中心格式有限体积法完成了拟压缩方法二维定常不可压euler方程的推导和流动计算程序的编写。
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