aerosandbox.library.airfoils# Module Contents# Functions# diamond_airfoil(t_over_c[, n_points_per_panel]) aerosandbox.library.airfoils.diamond_airfoil(t_over_c, n_points_per_panel=2)[source]# Parameters: t_over_c (float) – Return type: aerosandbox.geometry.airfoil.Airfoil