XFLR5 6.10.03

A free analysis tool for airfoils, wings and planes
XFLR5 is a free and open source analysis tool for airfoils, wings and planes operating at low Reynolds Numbers.

XFLR5 has a non-linear lifting line method for standalone wings and a two vortex lattice for the analysis of aerodynamic performance of wings.

last updated on:
April 18th, 2014, 7:55 GMT
file size:
10.3 MB
price:
FREE!
developed by:
Andre Deperrois
license type:
GPL 
operating system(s):
Mac OS X
binary format:
Universal Binary
category:
Home \ Math/Scientific

FREE!

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user rating 4

2.8/5
 

0/5

7 Screenshots
XFLR5XFLR5XFLR5XFLR5XFLR5XFLR5XFLR5
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
read full changelog

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