1) RANS/LES hybrid method
RANS/LES混合方法
1.
RANS/LES hybrid methods are developed on the basis of shear stress transport and weakly nonlinear k-ω models with compressible corrections.
在剪切应力输运和弱非线性k-ω模式中引入压缩性修正,并在此基础上构造RANS/LES混合方法,对包含丰富流动结构和复杂流动机理的导弹类超声速底部流场进行数值分析,发现压缩性修正可更好地描述流场特征,适于具有较强压缩性效应流动的数值分析;混合方法捕捉到丰富的流动现象及非定常特性。
2) hybrid RANS/LES
混合RANS/LES
1.
Unsteady flowfields are calculated by hybrid RANS/LES method.
采用混合RANS/LES方法对非定常流场进行数值模拟,考虑了凹腔的长深比和后缘角度两个关键参数。
2.
Calculations are carried out using the hybrid RANS/LES method to predict unsteady state flowfields.
采用混合RANS／LES方法对非定常流场进行数值模拟,考虑了凹腔的长深比和后缘角度两个关键参数。
3.
Calculations used hybrid RANS/LES method to predict unsteady state flow fields.
应用混合RANS/LES方法预报非定常流场,该模型很好地捕捉到了非定常大尺度结构并揭示了凹腔剪切层的演化。
3) Dynamic hybrid RANS/LES approach
动力混合RANS/LES
1.
Dynamic hybrid RANS/LES approach based on Me.
本文主要通过动力混合RANS/LES方法对二维超声速支板绕流以及喷射流场机理进行数值仿真研究。
4) LES/FWH hybrid method
LES/FWH混合方法
5) LES method
LES方法
1.
Three-dimensional numerical simulation of the flow past a circular cylinder based on LES method;
基于LES方法圆柱绕流三维数值模拟
2.
Three-dimensional numerical simulation of the flow past a circular cylinder based on LES method
基于LES方法圆柱绕流三维数值模拟(英文)
6) RANS equations
RANS方程
1.
The viscous flow between the wing-tip and the wall is simulated by solving the RANS equations of incompressible fluid.
本文通过求解不可压缩流体RANS方程 ,对机翼翼端与固壁之间隙流动进行了数值模拟。
2.
The incompressible RANS equations were solved by using Chorin s artificial compressibility method and the approximate factorization technique.
通过求解不可压缩流体RANS方程,数值模拟带端板三维地效应翼的性能及周围流场。
3.
The performance and flows of 2-D Wing-In-Ground Effect are numerically simulated by solving RANS equations using an implicit finite difference method.
本研究以隐式差分方法求解不可压RANS方程，对二维地效应翼的性能及周围流场进行数值模拟。
补充资料：[3-(aminosulfonyl)-4-chloro-N-(2.3-dihydro-2-methyl-1H-indol-1-yl)benzamide]
分子式：C16H16ClN3O3S
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条