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.

(goe282-il) GOE 282 (DAIMLER XIII) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 282 (DAIMLER XIII) airfoil Max thickness 9.1% at 19.9% chord Max camber 5% at 39.9% chord Max Cl/Cd 94.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe142-il) GOE 142 (MVA H.19) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 142 (MVA H.19) airfoil Max thickness 6.2% at 24.9% chord Max camber 3.8% at 34.9% chord Max Cl/Cd 94.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe427-il) GOE 427 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 427 airfoil Max thickness 4.6% at 20% chord Max camber 5.4% at 40% chord Max Cl/Cd 94.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e329-il) EPPLER 329 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E329 flying wing airfoil Max thickness 13.5% at 30.6% chord Max camber 3.5% at 25.7% chord Max Cl/Cd 94.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(s822-nr) NREL's S822 Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	NREL HAWT airfoil S822 tip 16.0% Dia=2 to 10 m Re=6.0E+5 Clmax(S)=1.00 Clmax(R)=0.98 Restrained max lift coef Max thickness 16% at 39.2% chord Max camber 1.8% at 59.5% chord Max Cl/Cd 94.7 at Re# 500,000 Source NWTC National WInd Technology Center

(goe408-il) GOE 408 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 408 airfoil Max thickness 7.8% at 30% chord Max camber 4.1% at 30% chord Max Cl/Cd 94.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(mh32-il) MH 32 8.7%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 32 for F3E and F3B Max thickness 8.7% at 30.2% chord Max camber 2.3% at 45.7% chord Max Cl/Cd 94.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe590-il) GOE 590 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 590 airfoil Max thickness 5.7% at 30% chord Max camber 4% at 30% chord Max Cl/Cd 94.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe629-il) GOE 629 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 629 airfoil Max thickness 13.6% at 29.4% chord Max camber 2.8% at 39.4% chord Max Cl/Cd 94.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(coanda3-il) Coanda 3		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Coanda 3 airfoil Max thickness 7% at 30% chord Max camber 2.9% at 40% chord Max Cl/Cd 94.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database