A free analysis tool for airfoils, wings and planes
XFLR5 has a non-linear lifting line method for standalone wings and a two vortex lattice for the analysis of aerodynamic performance of wings.
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What's New in This Release:
- Corrected the incorrect calculation of the mid camber line of foil with flaps
- Corrected the crash bug when calculating a wing with flaps using the LLT method
- Corrected the crash bug when deleting foils from the manage dialog box