Data code and source diagram of airfoil optimization design

These data are matlab codes for drawing pressure curves of two airfoils at different angles of attack, and various source figures, including the airfoil shape before and after treatment figure, the comparison curves of lift coefficient figure, the variation of lift-drag ratio coefficient with incoming wind speed under different attack angles figure,the variation of airfoil lift-drag ratio with attack angle at different incoming wind speeds figure and the pressure difference curves of two airfoils at different attack angles figure.

本数据集包含用于绘制两种翼型在不同攻角下压力曲线的 Matlab 代码，以及包括处理前后的翼型形状图、升力系数对比曲线图、不同攻角下来流风速下的升阻比系数变化图、不同来流风速下攻角变化时的翼型升阻比变化图，以及两种翼型在不同攻角下的压力差曲线图等多种来源图像。