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14.2 > Academic > xfoil (6.99)

XFOIL is an interactive program for the design and analysis of subsonic
isolated airfoils. It consists of a collection of menu-driven routines
which perform various useful functions, such as viscous (or inviscid)
analysis of an existing airfoil, airfoil design and redesign by
interactive modification of surface speed distributions or geometric
parameters, blending of airfoils, writing and reading of airfoil
coordinates and polar save files, and plotting of geometry, pressure
distributions, and multiple polars.

Maintained by: Daniel Prosser
Keywords: aerodynamics,airfoil,flight,aircraft
ChangeLog: xfoil

Homepage:
http://web.mit.edu/drela/Public/web/xfoil/

Source Downloads:
xfoil6.99.tgz (8d6270fc4341d299a426b3ad41be9cc4)

Download SlackBuild:
xfoil.tar.gz
xfoil.tar.gz.asc (FAQ)

(the SlackBuild does not include the source)

Validated for Slackware 14.2

See our HOWTO for instructions on how to use the contents of this repository.

Access to the repository is available via:
ftp git cgit http rsync

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