AeroFoil is an efficient and comprehensive program written in Visual Basic. AeroFoil uses the vortex panel method and integral boundary layer equations to calculate drag, lift, and airfoil pitching moment at different angles of attack. Direct comparisons of up to three airfoils at a time may be performed.
v1.5 [Oct 26, 2009]
- Available as a 64 bit (x64) executable.
- Source code updated for the wxWidgets 2.9.0 framework.
- Project updated for Visual Studio 2010.
- Multibyte strings have been removed in favour of Unicode.
- UPX compression has been removed due to lack of a 64 bit Windows packer (memory usage remains the same).
