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.

(e582-il) EPPLER 582 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E582 sailplane airfoil Max thickness 14.7% at 37.8% chord Max camber 4.2% at 43.1% chord Max Cl/Cd 112 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e855-il) EPPLER 855 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E855 propeller airfoil Max thickness 15.7% at 32.2% chord Max camber 3.7% at 50.6% chord Max Cl/Cd 112 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e201-il) E201 (11.88%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E201 low Reynolds number airfoil Max thickness 11.9% at 30.8% chord Max camber 2.6% at 49.4% chord Max Cl/Cd 112 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe492-il) GOE 492 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 492 airfoil Max thickness 6.2% at 29.9% chord Max camber 3.4% at 49.9% chord Max Cl/Cd 112 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx75141-il) WORTMANN FX 75-141		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 75-141 airfoil Max thickness 14.1% at 37.1% chord Max camber 3.4% at 53.3% chord Max Cl/Cd 111.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(a18-il) A18 (original)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Archer A18 F1C free flight airfoil(original) Max thickness 7.3% at 30% chord Max camber 3.9% at 45% chord Max Cl/Cd 111.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e694-il) EPPLER 694 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E694 sailplane airfoil Max thickness 15.4% at 40.4% chord Max camber 4.9% at 59.2% chord Max Cl/Cd 111.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e435-il) EPPLER 435 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E435 sailplane airfoil Max thickness 16.2% at 40.9% chord Max camber 4.4% at 56.2% chord Max Cl/Cd 111.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe446-il) GOE 446 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 446 airfoil Max thickness 12.9% at 29.7% chord Max camber 6.3% at 39.7% chord Max Cl/Cd 111.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(sa7025-il) SA7025		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig / Ashok Gopalarathnam SA7025 low Reynolds number airfoil Max thickness 8% at 29.2% chord Max camber 3.6% at 43.2% chord Max Cl/Cd 111.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database