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Lift calculator for NACA 4-digit, NACA 5-digit, and User defined airfoils
The Airfoil Lift app calculates the Coefficient of Lift (CL) for three different types of airfoils, NACA 4-digit shapes, NACA 5-digit shapes and user defined shapes. The app calculates the pressure distribution for both the top and bottom surfaces and the total Coefficient of Lift (CL). The app uses the Vortex Panel numerical method. Shape location points are also given so the user can copy and paste them into other graphic programs. The app can be used on both tablets and phones.What's New in the Latest Version 1.1.16
Last updated on Sep 11, 2021
icons update
64 bit version only
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Airfoil Lift
1.1.16 by Kurt Gramoll
Sep 11, 2021