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  • UIUC Airfoil Coordinates Database
    Included below are coordinates for approximately 1,650 airfoils (Version 2 0) The UIUC Airfoil Data Site gives some background on the database The airfoils are listed alphabetically by the airfoil filename (which is usually close to the airfoil name) Answers to frequently asked questions are posted here Airfoils FAQ and for the most recent changes see the update history
  • UIUC Airfoil Data Site - University of Illinois Urbana-Champaign
    The UIUC Airfoil Data Site is a collection of airfoil coordinates and airfoil related links The UIUC Airfoil Coordinates Database includes the airfoils, and they cover a wide range of applications from low Reynolds number airfoils for UAVs and model aircraft to jet transports and wind turbines Originally the site included mostly low Reynolds number airfoils (about 160), but in December 1995
  • UIUC Applied Aerodynamics Group
    UIUC LSATs airfoil data from Volumes 1-4, and 6 are here The UIUC Airfoil Data Site includes airfoil coordinates for approximately 1,650 airfoils Also useful is The Incomplete Guide to Airfoil Usage compiled and maintained by Dave Lednicer The guide includes a listing of what airfoils have been used on approximately 7,261 aircraft
  • Airfoil Updates - University of Illinois Urbana-Champaign
    Coordinates for these airfoils were first included in LSATS Vol 5 but somehow they slipped by their inclusion here in the airfoil coordinates database The airfoils are in the updates directory
  • UIUC Airfoil Coordinates Database (References)
    The airfoil he thought should be 10-11% thick and should not build up speed as quickly as the S3021 or E205 (which are both nearly flat-bottomed) As a result of this discussion, the S7055 was designed to fill this niche
  • UIUC Airfoil Coordinates Database (References)
    During the Princeton airfoil tests, several attempts were made to design an F3B airfoil (hot thermal duration airfoil) that out-performed the RG15, which was then among the best During the design process at Princeton, the objective was to develop an airfoil with lower drag everywhere In hindsight that objective is not physically possible To improve on the RG-15 performance requires making
  • UIUC APA - Links - University of Illinois Urbana-Champaign
    UIUC Airfoil Data Site - Airfoil coordinates and links UIUC Low-Speed Airfoil Tests - Low Reynolds number aerodynamics UIUC Propeller Database - Low Reynolds number propeller performance The Incomplete Guide to Airfoil Usage - Airfoils used on aircraft database Selig Publications PROFOIL-WWW for airfoil design on the web UIUC Aerospace
  • UIUC APA - LSATs
    The goals of the UIUC Low-Speed Airfoil Tests (UIUC LSATs) program are to design, analyze and wind tunnel test airfoils for low Reynolds number applications The UIUC Applied Aerodynamics group has been a leader in this research area with new airfoil designs being applied to unmanned aerial vehicles, small wind turbines, model aircraft and many other applications Over 200 low Reynolds number
  • UIUC Airfoil Coordinates Database (References)
    The new S4083 was designed for R C handlaunch competition Since the pilot (in the U S ) is allowed to change gliders during a handlaunch contest, then a suite of wings should be used: a low-speed wing, moderate-speed wing, and a high-speed wing The S4083 should prove best for the moderate to high-speed wing case
  • The Incomplete Guide to Airfoil Usage
    Something like "? x%" indicates that the airfoil is unknown, but sources indicate that the airfoil has a x% thickness to chord ratio Lastly, airfoil designations separated by slashes, , indicates that the wing design transitions from one airfoil to the next





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