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rans

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

  • The RANS equations method for aerodynamic numerical simulation of a high lift configuration in 2D and 3D cases, the results of computation and their comparisons with experimental data are investigated in detail.
    深入研究了二维和三维高升力外形空气动力数值模拟计算的雷诺平均NS(RANS)方程方法、计算结果、以及它们和实验数据的比较。
  • The investigation illustrated that the aerodynamic lift and pitching moment of wing can be predicted accurately by CFD based on RANS approach with comparison to model tests.
    结果表明与模型试验数据相比,基于RANS方程的CFD方法能够准确预报机翼的气动升力和力矩。
  • Propeller cavitation research by an unstructured grid based RANS solver
    基于非结构网格RANS方法螺旋桨空化研究
  • 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。
  • 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。
  • 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。
  • The algorithm is implemented in a viscous calculation based on a Reynolds-Averaged Navier-Stokes ( RANS) equation solver considering the effect of turbulence. A prior solution of wall detachment point and bubble length is not required. They are simulated by a cavitation model.
    提出的汽蚀模型和算法耦合了考虑紊流粘性效应的Reynolds-averagedNavier-Stokes方程求解方法,可以自动模拟空泡起始点、空泡长度和汽蚀空泡形状。
  • 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。
  • Besides, based on RANS method, a numerical calculation has been carried for simulating the above complex physical phenomenon.
    基于RANS方法,对上述复杂物理现象进行了数值模拟。
  • A Method Based on Low Dissipation Roe Scheme and RANS Equations for Predicting BVI Noise of Helicopter Rotor in Forward Flight
    低耗散格式在旋翼前飞气动噪声预测中的应用研究