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.

(fx80080-il) WORTMANN FX 80-080		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 80-080 airfoil Max thickness 8.1% at 40.2% chord Max camber 2.2% at 50% chord Max Cl/Cd 123.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(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 123.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e560-il) EPPLER 560 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E560 general aviation airfoil Max thickness 16.1% at 24% chord Max camber 4.9% at 51.1% chord Max Cl/Cd 123.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe335-il) GOE 335 (D.F.W.) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 335 (D.F.W.) airfoil Max thickness 6.9% at 20% chord Max camber 4.8% at 40% chord Max Cl/Cd 123.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe316-il) GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 316 (Hansa-Brandenburg IV.5) airfoil Max thickness 9.1% at 29.9% chord Max camber 4.2% at 29.9% chord Max Cl/Cd 123.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(eiffel385-il) Eiffel 385 (S.T. Ae)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eiffel 385 (S.T. Ae) airfoil Max thickness 13.4% at 20% chord Max camber 4.4% at 50% chord Max Cl/Cd 123.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe361-il) GOE 361 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 361 airfoil Max thickness 6.8% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 123.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe155-il) GOE 155 (SSW D.1) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 155 (SSW D.1) airfoil Max thickness 7% at 29.9% chord Max camber 5.3% at 39.9% chord Max Cl/Cd 123.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe322-il) GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 322 (Hansa-Brandenburg IV.1) airfoil Max thickness 13.1% at 29.8% chord Max camber 6% at 29.8% chord Max Cl/Cd 123.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s9037-il) S9037 (9%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S9037 (9%) low Reynolds number airfoil used on the Opus R/C sailplane Max thickness 9% at 28.5% chord Max camber 3.3% at 42.4% chord Max Cl/Cd 123.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database