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.

(eh3012-il) EH 3.0/12		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	John Yost EH 3.0/12 for tailless R/C aircraft Max thickness 12% at 30% chord Max camber 2.9% at 25% chord Max Cl/Cd 93.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e231-il) E231		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E231 R/C sailplane airfoil Max thickness 12.3% at 39.4% chord Max camber 2.5% at 39.4% chord Max Cl/Cd 93.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e555-il) EPPLER 555 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E555 general aviation airfoil Max thickness 16% at 31.9% chord Max camber 2.6% at 67.4% chord Max Cl/Cd 93.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe484-il) GOE 484 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 484 airfoil Max thickness 6.3% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 93.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe114-il) GOE 114 (MVA MK.1) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 114 (MVA MK.1) airfoil Max thickness 9.6% at 29.7% chord Max camber 3.5% at 49.7% chord Max Cl/Cd 93.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(e748-il) EPPLER 748 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E748 sailplane airfoil Max thickness 19.7% at 27.4% chord Max camber 4.6% at 54.9% chord Max Cl/Cd 93.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(raf31-il) RAF 31 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-31 airfoil Max thickness 12.7% at 30% chord Max camber 2.1% at 50% chord Max Cl/Cd 93.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe318-il) GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 318 (Hansa-Brandenburg VI.5) airfoil Max thickness 9.1% at 29.9% chord Max camber 4.3% at 29.9% chord Max Cl/Cd 93.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(rg15a213-il) RG 15A 2.5/13.0 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Rolf Girsberger RG 15A 2.5/13.0 airfoil Max thickness 13% at 30.2% chord Max camber 2.5% at 39.7% chord Max Cl/Cd 93.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(sd2083-il) SD2083 (9.0%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD2083 low Reynolds number airfoil Max thickness 9% at 35.2% chord Max camber 2.5% at 49.6% chord Max Cl/Cd 93.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database