Euler_solver

代码说明：

  基于有限体积法的naca0012翼型的无粘绕流计算(Calculation of airfoils based on the finite volume method naca0012 inviscid flow around)

文件列表：

Euler_solver
............\computeresult.f90,2310,2012-03-21
............\compute_d.f90,1668,2012-03-21
............\compute_q.f90,5087,2012-03-21
............\compute_r.f90,298,2012-03-21
............\compute_t.f90,456,2012-03-21
............\Cp_downwing_0.84_0.txt,3994,2012-02-16
............\Cp_downwing_0.8_1.25.txt,3994,2012-02-16
............\Cp_upwing_0.84_0.txt,3992,2012-02-16
............\Cp_upwing_0.8_1.25.txt,3992,2012-02-16
............\Dynamics of NACA0012 Airfoil_0.84_0.txt,149,2012-03-21
............\Dynamics of NACA0012 Airfoil_0.8_1.25.txt,149,2012-03-21
............\freeflow.ini,120,2012-02-16
............\global_mod.f90,706,2012-03-21
............\initialize.f90,2598,2012-03-21
............\integrate.f90,993,2012-03-21
............\iterate.f90,724,2012-03-21
............\main.dsp,4651,2012-02-16
............\main.dsw,531,2011-11-13
............\main.f90,265,2012-03-21
............\main.opt,46592,2012-06-25
............\main.plg,1195,2012-02-16
............\naca0012.grd,1055735,2008-11-06
............\outputdata.f90,1636,2012-03-21
............\readgrid.f90,1916,2012-03-21
............\Residual.txt,2550,2012-03-21
............\residualsmooth.f90,853,2012-03-21
............\Residual_0.84_0.txt,94550,2012-02-16
............\Residual_0.8_1.25.txt,116550,2012-02-16