Data code and source diagram of airfoil optimization design

Description

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.

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