Description

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 Version 1.1.15

This app has been updated by Apple to use the latest Apple signing certificate.