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.

(goe433-il) GOE 433 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 433 airfoil Max thickness 17.4% at 29.2% chord Max camber 4.8% at 49.2% chord Max Cl/Cd 89 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(rg15-il) RG-15 8.9%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Rolf Girsberger RG 15 low Reynolds number airfoil Max thickness 8.9% at 30.2% chord Max camber 1.8% at 39.7% chord Max Cl/Cd 89 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(c141f-il) LOCKHEED C-141 BL958.89 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Lockheed-Georgia C-141 transonic wing airfoils Max thickness 10% at 40.2% chord Max camber 2.3% at 45.1% chord Max Cl/Cd 89 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(sp4721la-po) SP4721LA		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	Saab-Pimenta High Performance low TE dB(A) noise 100 m Diameter Wind Turbine Main Airfoil in Quiet Mode of Operation Max thickness 21.4% at 34.8% chord Max camber 4.4% at 67.6% chord Max Cl/Cd 89 at Re# 500,000 Source Poli-Wind. University of Sao Paulo
(e1211-il) EPPLER 1211 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E1211 general aviation airfoil Max thickness 18% at 20.9% chord Max camber 4.4% at 37.7% chord Max Cl/Cd 89 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(fx60160-il) FX 60-160 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 60-160 airfoil Max thickness 15.6% at 40% chord Max camber 3.1% at 60% chord Max Cl/Cd 89 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ag36-il) AG36		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG36 airfoil Max thickness 8.2% at 27.9% chord Max camber 2.3% at 37% chord Max Cl/Cd 88.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(sa7036-il) SA7036		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig / Ashok Gopalarathnam SA7036 Max thickness 9.2% at 28.1% chord Max camber 2.6% at 42.1% chord Max Cl/Cd 88.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe593-il) GOE 593 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 593 airfoil Max thickness 11.9% at 30% chord Max camber 4.1% at 40% chord Max Cl/Cd 88.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e328-il) EPPLER 328 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E328 flying wing airfoil Max thickness 13.3% at 31.5% chord Max camber 3% at 22.1% chord Max Cl/Cd 88.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database