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.

(stcyr24-il) St. CYR 24 (Bartel 35-IIIC)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	St. CYR 24 (Bartel 35-IIIC) airfoil Max thickness 12.4% at 30% chord Max camber 5.9% at 40% chord Max Cl/Cd 89.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe199-il) GOE 199 (L.F.G. 5406) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 199 (L.F.G. 5406) airfoil Max thickness 7.3% at 30% chord Max camber 5.2% at 30% chord Max Cl/Cd 89.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e222-il) E222 (10.17%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E222 low Reynolds number airfoil Max thickness 10.2% at 31.1% chord Max camber 2.1% at 55.3% chord Max Cl/Cd 89.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(cr1-il) CURTISS CR-1 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Curtiss CR-1 general aviation airfoil Max thickness 12.2% at 24% chord Max camber 4.7% at 42% chord Max Cl/Cd 89.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(marske1-il) MARSKE XM-1D AIRFOIL (F14-3.0)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Marske XM-1D airfoil (F14-3.0) Max thickness 14% at 25.1% chord Max camber 3% at 25.1% chord Max Cl/Cd 89.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(fauvel-il) FAUVEL 14% AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Fauvel 14% flying wing airfoil Max thickness 14% at 25.2% chord Max camber 2.5% at 25.2% chord Max Cl/Cd 89.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe532-il) GOE 532 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 532 airfoil Max thickness 12.5% at 30% chord Max camber 4.8% at 40% chord Max Cl/Cd 89.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe702-il) GOE 702 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 702 airfoil Max thickness 16.6% at 19.4% chord Max camber 5.1% at 39.4% chord Max Cl/Cd 89.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(rhodesg32-il) Rhode St. Genese 32		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Rhode St. Genese 32 airfoil Max thickness 11.9% at 30% chord Max camber 3.9% at 40% chord Max Cl/Cd 89.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe490-il) GOE 490 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 490 airfoil Max thickness 8.8% at 19.9% chord Max camber 3.8% at 39.9% chord Max Cl/Cd 89.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database