文件名称:Euler_solver
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- 上传时间:2012-11-16
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文件大小:317.1kb
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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
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下载文件列表
Euler_solver/computeresult.f90
Euler_solver/compute_d.f90
Euler_solver/compute_q.f90
Euler_solver/compute_r.f90
Euler_solver/compute_t.f90
Euler_solver/Cp_downwing_0.84_0.txt
Euler_solver/Cp_downwing_0.8_1.25.txt
Euler_solver/Cp_upwing_0.84_0.txt
Euler_solver/Cp_upwing_0.8_1.25.txt
Euler_solver/Dynamics of NACA0012 Airfoil_0.84_0.txt
Euler_solver/Dynamics of NACA0012 Airfoil_0.8_1.25.txt
Euler_solver/freeflow.ini
Euler_solver/global_mod.f90
Euler_solver/initialize.f90
Euler_solver/integrate.f90
Euler_solver/iterate.f90
Euler_solver/main.dsp
Euler_solver/main.dsw
Euler_solver/main.f90
Euler_solver/main.opt
Euler_solver/main.plg
Euler_solver/naca0012.grd
Euler_solver/outputdata.f90
Euler_solver/readgrid.f90
Euler_solver/Residual.txt
Euler_solver/residualsmooth.f90
Euler_solver/Residual_0.84_0.txt
Euler_solver/Residual_0.8_1.25.txt
Euler_solver
Euler_solver/compute_d.f90
Euler_solver/compute_q.f90
Euler_solver/compute_r.f90
Euler_solver/compute_t.f90
Euler_solver/Cp_downwing_0.84_0.txt
Euler_solver/Cp_downwing_0.8_1.25.txt
Euler_solver/Cp_upwing_0.84_0.txt
Euler_solver/Cp_upwing_0.8_1.25.txt
Euler_solver/Dynamics of NACA0012 Airfoil_0.84_0.txt
Euler_solver/Dynamics of NACA0012 Airfoil_0.8_1.25.txt
Euler_solver/freeflow.ini
Euler_solver/global_mod.f90
Euler_solver/initialize.f90
Euler_solver/integrate.f90
Euler_solver/iterate.f90
Euler_solver/main.dsp
Euler_solver/main.dsw
Euler_solver/main.f90
Euler_solver/main.opt
Euler_solver/main.plg
Euler_solver/naca0012.grd
Euler_solver/outputdata.f90
Euler_solver/readgrid.f90
Euler_solver/Residual.txt
Euler_solver/residualsmooth.f90
Euler_solver/Residual_0.84_0.txt
Euler_solver/Residual_0.8_1.25.txt
Euler_solver
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