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款翼型在不同攻角下压力曲线的MATLAB代码，以及各类源图像素材，具体包括翼型处理前后的形态对比图、升力系数对比曲线图、不同攻角下升阻比系数随来流风速的变化曲线图、不同来流风速下翼型升阻比随攻角的变化曲线图，以及两款翼型在不同攻角下的压差曲线图。