Airfoil Tools
Search 1638 airfoils

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Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil database search

Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

(goe372-il) GOE 372 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 372 airfoil Max thickness 6.2% at 29.9% chord Max camber 4.3% at 39.9% chord Max Cl/Cd 108.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(mh18-il) MH 18 11.16%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 18 for F3D Pylon Racing Max thickness 11.1% at 36.8% chord Max camber 2.7% at 42.1% chord Max Cl/Cd 108.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe301-il) GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 301 (Friedrichshafen G 13) airfoil Max thickness 10% at 28.9% chord Max camber 6.5% at 39.9% chord Max Cl/Cd 108.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e212-il) E212 (10.55%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E212 low Reynolds number airfoil Max thickness 10.6% at 27.5% chord Max camber 2.5% at 61.3% chord Max Cl/Cd 108.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe476-il) GOE 476 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 476 airfoil Max thickness 14.5% at 29.5% chord Max camber 5.2% at 39.5% chord Max Cl/Cd 108.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(goe234-il) GOE 234 (MVA CA5) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 234 (MVA CA5) airfoil Max thickness 14.2% at 19.7% chord Max camber 9.2% at 49.7% chord Max Cl/Cd 108.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe425-il) GOE 425 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 425 airfoil Max thickness 16% at 29.3% chord Max camber 4.5% at 39.3% chord Max Cl/Cd 108.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe439-il) GOE 439 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 439 airfoil Max thickness 7.9% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 108.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e432-il) EPPLER 432 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E432 sailplane airfoil Max thickness 16% at 37.4% chord Max camber 4.5% at 37.4% chord Max Cl/Cd 108.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(k3311sm-il) K3311 (smoothed)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Leon Kincaid K3311 airfoil (smoothed) Max thickness 11% at 30.6% chord Max camber 3.2% at 41.6% chord Max Cl/Cd 108.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database