搜索资源列表
EXAM6
- 由两平行平板组成的突扩通道，尺寸如图所示。流动为层流。入口流速均匀，入口温度均匀，通道壁温均匀。分子粘性、密度已知，求：通道中流体的速度分布、温度分布、密度分布及压力场。-Formed by two parallel plates sudden expansion channel, size as shown. Flow is laminar flow. Uniform inlet velocity, inlet temperature uniformity, the channel wall
duct4
- duct.f computes a fully developed viscous laminar flow in a rectangular channel of aspect ratio b/a (=bar). solve the equation: d^2u/dx^2 + d^2u/dy^2 = -1, -a<x<a, -b<y<b method of discretisation: 3-point centered differences
simple
- 无限大平板间的层流流动Simple算法计算-Infinite plate laminar flow between the Simple algorithm
laminarflow
- How the laminar flow structure through the pipes ways
FLOW0
- 本程序是采用麦克马克方法编制的通用程序，可计算二维，三维，湍流，层流等复杂流场。-The program is compiled using a common method McCormack program calculates two-dimensional, three-dimensional, turbulent, laminar flow and other complex flow field.
NACA0012_Validation_Laminar
- validation paper for Laminar viscous Compressible flow, Over Naca 0012- validation paper for Laminar viscous Compressible flow, Over Naca 0012
996503102
- 空气动力学中壁面层流的计算文件，可以计算任一点的压强和速度等物理量，适用于薄壁-Wall laminar flow aerodynamics calculation file can be calculated at any point of the physical quantities such as pressure and speed, suitable for thin-walled
CavityFlow
- 带有盖移动速度流考虑模拟的一个盖子驱动下腔流是层流和不可压缩的牛顿流体压力校正方法用于以交错网格上解决的Navier Stokes方程-Simulating a Lid-Driven Cavity flow with a lid moving at speed uo Flow considered is laminar and of an incompressible Newtonian fluid Pressure correction method is used on a staggere
k_pohlhausen
- 已知翼型坐标及其各点的马赫数分布用波豪森近似方法求解层流附面层厚度-The known airfoil coordinates of its point of Mach number distribution wave the Stockhausen approximation method for solving laminar flow boundary layer thickness
order
- a function that classifies a flow according to the values of its Reynolds (Re) and Mach (Ma) numbers, such that if Re < 2000, the flow is laminar if 2000 < Re < 5000, the flow is transitional if Re > 5000, the flow is turbulent if M
BACKWARD_STEP01
- Incompressible laminar viscous flow past a backward facing step
NHT
- 本程序是计算传热学程序，可以模拟流动和传热的现象，已经验证过，没有任何问题。放心下载。该程序的特色是灵活性强不仅可以模拟层流也可以模拟湍流。-This is a forran-based program for simulation of numerical heat transfer ,it is flexible and applicable to a various field ,the most charateristic is that ,it integrate the phenom
2-_-Basic-Lattice-Boltzmann-(LB)
- Simple, yet simplistic, Lattice Boltzmann (LB) MATLAB implementation. D2H9, BGK, omega = 1, laminar flow in a 2D channel used as benchmark. Requires Image Processing Toolbox. The code is not optimized for memory nor for speed, i.e. not efficient
DUCT
- Laminar Flow In Duct:FVM (simple algoritm and power law scheme)
Bodyfitted_cylinder_FORTRAN
- 2d Laminar flow over a circular cylinder. 4th order 7 point DRP scheme is used.
2-cylinder(overset)
- Overset grid method for 2D laminar flow over two cylinder. high order discretization scheme is utilized to see the acoustic wave as well.
pablo
- Pablo is a pedagogical low-speed airfoil analysis program written in MATLAB. It uses a one way coupled inviscid + boundary layer model. The inviscid flow is solved using a Panel Method [1]. Three different kinds of singularity distributions can
LBGK_D2Q9_poiseuille_channel2D
- 二维通道层流，matlab实现，格子玻尔兹曼方法(Simple, yet simplistic, Lattice Boltzmann (LB) MATLAB implementation. D2H9, BGK, omega = 1, laminar flow in a 2D channel used as benchmark.)