


#Uiuc airfoil data series#
Selig, M.S., "Low Reynolds Number Airfoil Design," VKI Lecture Series - Low Reynolds Number Aerodynamics on Aircraft Including Applications in Emerging UAV Technology, von Karman Institute for Fluid Dynamics (VKI) Lecture Series, RTO/AVT-VKI-104, November 2003.and Selig, M.S., "Low Reynolds Number Airfoil Design and Wind Tunnel Testing at Princeton University," Lecture Notes in Engineering, edited by T.J. Afgan, Near-Wall Turbulence, Hemisphere Publishing Corp., New York, 1990. Zaric Memorial International Seminar, edited by S.J. and Smits, A.J., "The Dynamic Behavior of a Shock-Wave/Turbulent Boundary Layer Interaction," Zoran P. Mueller, Progress in Astronautics and Aeronautics Series, AIAA, Vol. Selig, M.S., Gopalaratham, A., Giguère, P., and Lyon, C.A., "Systematic Airfoil Design Studies at Low Reynolds Numbers," Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications, edited by T.J.Selig, M.S., Donovan, J.F., and Fraser, D.B., Airfoils at Low Speeds, SoarTech Publications, Virginia Beach, VA, 1989, 398 pages.

1, SoarTech Publications, Virginia Beach, VA, 1995, 292 pages.
#Uiuc airfoil data software#
PROPID - Wind Turbine Rotor Design and Analysis Software.Prof Selig's Research Group: UIUC Applied Aerodynamics Group.Welcome to, a database of shapes, data, and other information pertinent to 2D airfoil sections.305 Talbot Laboratory For More Information Various links to airfoils management websites

Serge Barth, Sergey Sobakin, Stéphane Combet, S other NACA (Realize your Naca airfoils), NM, MVR et NMR ( Nicolas Mathis+Marco Virgilio Ricci) Marcel Guwang, Matthieu Scherrer, Martin Hepperle, E. Hannes Delago, HL B.Horeni et J.Lnenka,Hans Meyer, Hammarskiöld-Mattias, Norbert Habe, Horten,Helmut Quabeck, Hartmut Siegmann, H other That airfoils are not included in the UIUC Airfoil Data Site and are into the " Pack de profils"ĭownload All the airfoils from these pages - 820 Ko ()ĭirk Pflug, Mark Drela, Delft University, DS airfoil(Joe WURTS) A commercial use is restricted by the designers copyright, Please contact the designer. The airfoils can be used by every private person.
