BigFoil Visual Catalog
Cl and Cd Data shown was computed by JavaFoil for a smooth airfoil at Re=6M, Mach=0.
Click on an airfoil image to go to it's page.
Aguerre
Althaus
Ayers
Baron
Barth
Boeing
Clark
Delft
Drela
Egglestone
Eiffel
Eppler
Girsberger
Gottingen
Gulfstream
Habbe
Hepperle
Horeni - Lnenka
Horten
Joukowsky
Leinauer
Lockheed
Lutz
Marske
Mathis
Mauk
Meyer
Midic
Molfino
NACA
NACA 4-digit
NACA 4-digit modified
NACA 5-digit
NACA 63-series
NACA 64-series
NACA 65-series
NACA 66-series
NACA 67-series
NACA/Munk
NASA
NPL
Onera
Pflug
Platon
Quabeck
RAE
RAF
Riblett 30-series
Riblett 35-series
Riblett 37-series
Riblett 40-series
Ritz
Scherrer
Selig et. al.
Sickinger
Siegmann
Sielemann
Sikorsky
Taylor
TsAGI
TsAGI B
Uncategorized
USA
Wick
Wortmann
Yost
Zutter