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flapping
- 使用非定常涡格法(UVLM)计算一种简单扑翼机的升力。对应文献Time Domain Modeling of Unsteady Aerodynamic Forces on a Flapping Airfoil -Eric Durand（MIT Master thesis）-Unsteady vortex lattice method (UVLM) a simple flapping wing machine lift. Corresponding literature Time Domain M
1D-Euler
- 用于求解一维气体动力学的欧拉方程代码，采用戈东诺夫格式，显式推进，可仿真非定常激波管-For solving one-dimensional Euler equations of gas dynamics code, using Godunov format, explicit advance, can simulate unsteady shock tube
kernel
- 本程序采用核函数法计算非定常情况下的非定常气动力，注意此方法与网格法是不同的，不用于网格法中的核函数-This program uses a kernel function method to calculate unsteady aerodynamic often unsteady case, note that this method is different from the grid method, grid method is not used in the kernel functi
DLM
- 计算升力面非定常气动力的偶极子网格法MATLAB程序-Matlab functions to calculate unsteady aerodynamic pressures on a lifting surface using doublet lattice method.
FEMfor-unsteady-problem
- 有限元法，求解unsteady stoke problem 和 LU decomposition solver-the finite elemental methods. the code for solving the unsteady stoke problem with LU decomposition solver for the linear qeuations system
GREATZER
- 模型数值验证非定常流体力学大作业孙晓峰老师-geritzer Numerical model validation unsteady hydrodynamic big job Sun Xiaofeng teacher
grizter
- gritzer模型数值验证非定常流体力学大作业孙晓峰老师-gritzer Numerical model validation unsteady hydrodynamic big job Sun Xiaofeng teacher
fluent-Get-Time-Step
- 通过设置特征长度和特征速度可以得到非定常计算的时间步长-It can be unsteady calculations by setting the characteristic length and velocity characteristics of the time step
PKmethod
- 运用西奥道生非定常气动力模型计算气动力，采用p-k法计算二元翼段的颤振临界速度(The aerodynamic force is calculated by the unsteady aerodynamic model of Theo road. The critical flutter velocity of the two element airfoil is calculated by the P-K method)
CFD2
- MATLAB程序，使用向后差分方法模拟一维非稳态导热(Simulation of one dimensional unsteady state heat conduction)