The source code for the program is offered under the GNU General Public License. Please feel free to download the code, read it, modify it, compile it and run it locally. -Parameter definitions: use_naca: logical, true if we want to ge

翼型在势流中的模拟，以求得其压力系数分布，升力系数等-Airfoil in potential flow in the simulation, with a view to obtaining the pressure coefficient distribution, the lift coefficient