搜索资源列表
MacCormack_1D_FORTRAN
- MacCormack格式，fortran计算一维流动的源代码-MacCormack format, fortran calculate the source code of one-dimensional flow
CFD_CSharp
- cfd经典问题C源代码：一维黎曼问题；一维可压N-S方程；二维斜激波刚壁反射；二维泊萧叶黏性流动；有限体积法求解库塔流-Riemann problem a compressible N-S equations of two-dimensional oblique shock wave reflection stiffness 2D Poiseuille viscous flow finite volume method to solve the Kuta flow
CFD_CSharp
- cfd经典问题C源代码：一维黎曼问题；一维可压N-S方程；二维斜激波刚壁反射；二维泊萧叶黏性流动；有限体积法求解库塔流-Riemann problem a compressible N-S equations of two-dimensional oblique shock wave reflection stiffness 2D Poiseuille viscous flow finite volume method to solve the Kuta flow
code
- 一维喷管流动数值模拟,用的fortran语言，对于上流体力学的同学很有帮助-Numerical simulation of one-dimensional nozzle flow, using fortran language is helpful for students on the hydrodynamics
RIFTUD
- 一维fortran涡轮设计程序。输入包括功率，质量流量，入口温度和压力，转速。设计变量包括静子出口角，转子半径比和转子出口切向速度分布。损失由内部损失模型计算。程序输出包括直径，效率，温度，压力，速度，流动角。-1D radial compressor design fortran program.Input design requirements are power, mass flow rate, inlet temperature and pressure, and rotat
solution-
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解 7.3节 亚声速—超声速等熵喷管流动的CFD解法 -CFD solution supersonic isentropic nozzle flow- Anderson " Computational Fluid Dynamics and Its Applications," Chapter VII of the quasi one-dimensional nozzle flow numerical solution of
Upwind1d
- 一维可压缩黏性流动是气体动力学中最经典的黏性流动问题，采用迎风型差分算法进行数值求解。这里给出了计算一维可压缩黏性流动问题的计算程序。-One-dimensional compressible viscous flow is the most classic aerodynamic viscous flow problems, using upwind difference algorithm for numerical solving. Here is a computer program t
fvm_MAC_couette
- 不可压缩黏性流动的典型流动，有解析解，可以用来检验数值算法计算精度和可靠性。采用有限体积算法一阶迎风型离散格式进行数值求解。这里给出了计算二维不可压缩黏性流体流动问题计算程序，供大家学习参考。-A typical flow of an incompressible viscous flow, there are analytical solution, numerical algorithms can be used to test the accuracy and reliability. F
FLUX.f90.tar
- CFD计算中，构造流动通量的一种方法，利用了特征分裂的二维计算-a method constructing flux in CFD
B
- 一维可压缩黏性流动是气体动力学中最经典的黏性流动问题，对它采用迎风型 差分算法进行数值求解。-One-dimensional viscous compressible gas flow dynamics of the most classic viscous flow problems, use it upwind difference algorithm for numerical solving.