XFOIL

Last updated
XFOIL
Written in Fortran
License GPL
Website web.mit.edu/drela/Public/web/xfoil

XFOIL is an interactive program for the design and analysis of subsonic isolated airfoils. Given the coordinates specifying the shape of a 2D airfoil, Reynolds and Mach numbers, XFOIL can calculate the pressure distribution on the airfoil and hence lift and drag characteristics. The program also allows inverse design - it will vary an airfoil shape to achieve the desired parameters. It is released under the GNU GPL.

Contents

History

XFOIL was first developed by Mark Drela at MIT as a design tool for the MIT Daedalus project in the 1980s. [1] It was further developed in collaboration with Harold Youngren. The current version is 6.99, released in December 2013. Despite its vintage, it is still widely used. [2]

XFOIL is written in FORTRAN.

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References

  1. "MIT Aero-Astro Magazine - Mark Drela Profile".
  2. "Aerodynamics and Aircraft Design Software". Archived from the original on June 8, 2010. Retrieved August 3, 2010.
  3. http://www.mathworks.com/matlabcentral/fileexchange/50070-xfoil-for-matlab.html
  4. http://www.mh-aerotools.de/airfoils/javafoil.htm