rans

英

美 [rænz]

网络  雷诺平均; 雷诺平均法; 斯托克斯; 雷诺平均模拟

双语例句

• For this purpose, several types of manpowered seawater pulverization chamber were designed in this thesis with simulation on the inner gas-granule flow field through RANS equation and DPM model.
  本文即是依据这一目的设计几种结构形式的人工海水雾化室，将RANS方程与DPM模型相结合对其内部的气液两相流流场进行数值模拟。
• Research on the RANS/ LES hybrid method for supersonic/ hypersonic turbulence flow
  超声速湍流流场的RANS/LES混合计算方法研究
• The paper takes one 1000 tons hybrid monohull as a object of the research and the paper will use potential method and RANS method to compute the hydrodynamic coefficients of two-dimensional stations and the three-dimensional hull.
  本文以某千吨级单体复合船型为研究对象，利用势流理论方法和RANS方法分别对二维横剖段和三维船体的水动力系数进行了计算。
• A finite-volume method of solving incompressible Reynolds-averaged Navier-Stokes ( RANS) equations was used for the numerical simulation of three-dimensional viscous flow around the vehicle in body-fitted coordinate system. The ( k-ε) turbulence model was employed to close the RANS equations.
  在三维贴体坐标系下，采用有限体积法求解不可压缩的雷诺平均（RANS）方程，使用标准k-ε湍流模型实现方程的封闭，数值模拟了艇体周围的粘性流场。
• In addition, the flow control mechanism of suction/ blowing, synthetic jet was investigated and RANS/ LES hybrid methods was utilized to study there-dimentional airfoil.
  研究分析了吸/吹气、合成射流流动控制机理，并采用了RANS/LES混合方法对三维翼型绕流进行了研究。
• Governing equation is RANS equation with standard κ-ε model, the discrete method is a finite volume method based on a finite element approach of representing the geometry.
  本问题用RANS方程和κ-ε模型联合求解，离散化是建立在用有限元方法描述几何图形的有限体积法；同时，利用多重网络技术加快收敛速度；
• The detailed research is including: Firstly, a two dimensional incompressible RANS model is established. Several existing viscous models are studied for the suitability to describe the synthetic jet phenomena.
  具体的研究内容有：第一，基于二维不可压缩RANS方程建立数值模型，研究了现有几种湍流模型在描述合成射流现象时的适用性。
• Numerical study and nonlinear analysis of supersonic mixing layer in Dual-Combustor Ramjet is conducted in this thesis.2-dimension supersonic combustor flow field is studied by RANS simulation method.
  本文针对双燃烧室冲压发动机超声速混合层进行了数值模拟和非线性分析。
• In the coupling procedure, the unsteady cavity flow field is first computed solving RANS equations.
  耦合过程中，首先求解RANS方程来得到非定常的空腔流场。
• Study on Supersonic Base Flow Using RANS/ LES Methods
  用RANS/LES混合方法研究超声速底部流动