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.

(goe795sm-il) GOE 795 smoothed		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 795 airfoil (smoothed) Max thickness 8% at 30.9% chord Max camber 2.4% at 43.5% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(s1221-il) S1221 w/o flap		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S1221 airfoil Max thickness 12.1% at 21.8% chord Max camber 4.9% at 49.1% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe376-il) GOE 376 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 376 airfoil Max thickness 6.6% at 30% chord Max camber 5% at 30% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe178-il) GOE 178 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 178 airfoil Max thickness 8.5% at 30% chord Max camber 4.4% at 30% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e433-il) EPPLER 433 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E433 sailplane airfoil Max thickness 14.2% at 42.6% chord Max camber 3.9% at 42.6% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(fx83w160-il) FX 83-W-160		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 83-W-160 airfoil for use on wind turbines (W) Max thickness 16.1% at 37.1% chord Max camber 3.9% at 62.9% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe592-il) GOE 592 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 592 airfoil Max thickness 14.3% at 29.7% chord Max camber 7.5% at 39.7% chord Max Cl/Cd 76.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e591-il) E591		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E591 airfoil Max thickness 15.7% at 25% chord Max camber 6% at 52.3% chord Max Cl/Cd 76.5 at Re# 200,000 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 76.4 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe381-il) GOE 381 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 381 airfoil Max thickness 6.4% at 30% chord Max camber 5.8% at 30% chord Max Cl/Cd 76.4 at Re# 200,000 Source UIUC Airfoil Coordinates Database