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.

(goe613-il) GOE 613 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 613 airfoil Max thickness 10.3% at 30% chord Max camber 4.1% at 40% chord Max Cl/Cd 72.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe623-il) GOE 623 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 623 airfoil Max thickness 12% at 30% chord Max camber 3.8% at 40% chord Max Cl/Cd 72.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe286-il) GOE 286 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 286 airfoil Max thickness 9.4% at 29.9% chord Max camber 4.1% at 29.9% chord Max Cl/Cd 72.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(m18-il) NACA M18 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-18 airfoil Max thickness 12% at 30% chord Max camber 4.1% at 30% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(ah81131-il) AH 81-131		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 81-131 airfoil Max thickness 13.1% at 40.2% chord Max camber 2.8% at 40.2% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe385-il) GOE 385 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 385 airfoil Max thickness 9.9% at 29.9% chord Max camber 4.1% at 29.9% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e598-il) EPPLER 598 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E598 airfoil Max thickness 11.1% at 24.2% chord Max camber 4.5% at 34.4% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(m15-il) NACA M15 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-15 airfoil Max thickness 12% at 30% chord Max camber 3.8% at 30% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(clarkz-il) CLARK Z AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	CLARK Z airfoil Max thickness 11.8% at 30% chord Max camber 4% at 40% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe615-il) GOE 615 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 615 airfoil Max thickness 13.7% at 29.7% chord Max camber 5.6% at 39.7% chord Max Cl/Cd 72.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database

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