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xfoil

program for the design and analysis of subsonic airfoils

program for the design and analysis of subsonic airfoils
from version 6.97.dfsg-5

Description

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 specification of
    a surface speed distribution via screen cursor or mouse
  - Airfoil redesign by interactive specification of new geometric
    parameters
  - Blending of airfoils
  - Drag polar calculation with fixed or varying Reynolds and/or
    Mach numbers.
  - Plotting of geometry, pressure distributions, and polars

Homepage

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


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