Airfoil Tools
Search 1638 airfoils

You have 0 airfoils loaded.
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.

(goe448-il) GOE 448 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 448 airfoil Max thickness 12.9% at 29.8% chord Max camber 10.5% at 39.8% chord Max Cl/Cd 162 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(saratov-il) SARATOV AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Saratov R/C sailplane airfoil Max thickness 9.2% at 15% chord Max camber 9.8% at 40% chord Max Cl/Cd 161.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe464-il) GOE 464 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 464 airfoil Max thickness 7.7% at 7.4% chord Max camber 9.9% at 29.9% chord Max Cl/Cd 151.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe802a-il) GOE 802 A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 802 A airfoil Max thickness 9.8% at 30% chord Max camber 6.1% at 40% chord Max Cl/Cd 149.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e379-il) EPPLER 379 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E379 ultralight airfoil Max thickness 2.2% at 5.8% chord Max camber 8% at 31.8% chord Max Cl/Cd 117.8 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(e63-il) E63 (4.25%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E63 low Reynolds number airfoil Max thickness 4.3% at 22.8% chord Max camber 5.3% at 50.5% chord Max Cl/Cd 112.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e61-il) E61 (5.64%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E61 low Reynolds number airfoil Max thickness 5.7% at 23.8% chord Max camber 6.4% at 51% chord Max Cl/Cd 112.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e61-il) E61 (5.64%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E61 low Reynolds number airfoil Max thickness 5.7% at 23.8% chord Max camber 6.4% at 51% chord Max Cl/Cd 110.8 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e63-il) E63 (4.25%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E63 low Reynolds number airfoil Max thickness 4.3% at 22.8% chord Max camber 5.3% at 50.5% chord Max Cl/Cd 110 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e71-il) E71 (5.15%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E71 low Reynolds number airfoil Max thickness 5.2% at 25.7% chord Max camber 4.4% at 54% chord Max Cl/Cd 108.4 at Re# 200,000 Source UIUC Airfoil Coordinates Database