CST_airfoil_fitting

代码说明：

  一个拟合CST曲线的程序，用来做翼型优化使用（也可以用到其它曲线拟合上）。 首先读入一个翼型数据，反求这个翼型的6*2个控制参数。通过这修改这个12个控制参数（其中的任意几个），来达到生成新的翼型的目的。(使用了NASA0714翼型作为例子 )(it is a code for airfoil curves fitting, which based on CST formula.Firstly, the program read a airfoil data,then the program will output 12 parameters which can fit the airfoil. you can change those parameters to get new airfoil shape.（there give a example of NASA 0714 airfoil fitting）)

文件列表：

CST方法拟合翼型
...............\NASA SC(2)-0714.dat,4715,2014-12-05
...............\NASA SC(2)-0714_coeff.dat,384,2014-12-06
...............\NASA SC(2)-0714_coord.dat,12484,2014-12-06
...............\_ArCoeff.h,2279,2014-12-05
...............\_CST.cpp,582,2014-12-06
...............\_CSTMainFormula.h,2316,2014-12-05
...............\_CSTPolynome.h,621,2014-12-05
...............\_GetCoeff.h,4351,2014-12-06
...............\_GetNewCoord.h,3178,2014-12-06
...............\_Matrix.cpp,8451,2014-12-04
...............\_Matrix.h,1274,2014-12-03