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- 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