The latest version of the manual will always be available from the X‑Plane Developer web site. This is version 11.50 of the manual to Airfoil Maker. Last updated: 16 August 2021 About This Manual Stall Minimum and Maximum Angle of Attack.Coefficient of Moment at High-Alpha Change Point.Coefficient of Moment at Low-Alpha Change Point.Coefficient of Moment High-Alpha Change Point.Coefficient of Moment Low-Alpha Change Point.Coefficient of Drag at Angle of Attack of 10 Degrees.
Coefficient of Lift at Which Minimum Drag Occurs.Coefficient of Lift Drop from Stall to 20 Degrees.Coefficient of Lift Curvature After the Stall.Coefficient of Lift Immediate Drop at Stall.Coefficient of Lift Curvature Near the Stall.
0 kommentar(er)
