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.

(goe386-il) GOE 386 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 386 airfoil Max thickness 20.3% at 29% chord Max camber 5.4% at 39% chord Source UIUC Airfoil Coordinates Database
(goe449-il) GOE 449 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 449 airfoil Max thickness 17% at 30% chord Max camber 5.4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe604-il) GOE 604 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 604 airfoil Max thickness 17.8% at 29.3% chord Max camber 5.4% at 29.3% chord Source UIUC Airfoil Coordinates Database
(goe182-il) GOE 182 (MVA H.27) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 182 (MVA H.27) airfoil Max thickness 9.5% at 19.9% chord Max camber 5.3% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe647-il) GOE 647 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 647 airfoil Max thickness 16.2% at 19.5% chord Max camber 5.3% at 39.4% chord Source UIUC Airfoil Coordinates Database
(goe184-il) GOE 184 (MVA H.29) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 184 (MVA H.29) airfoil Max thickness 8.3% at 19.9% chord Max camber 5.3% at 39.9% chord Source UIUC Airfoil Coordinates Database
(e398-il) EPPLER 398 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E398 human powered aircraft airfoil Max thickness 14.2% at 29.6% chord Max camber 5.3% at 50.9% chord Source UIUC Airfoil Coordinates Database
(e397-il) EPPLER 397 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E397 human powered aircraft airfoil Max thickness 13.5% at 29.4% chord Max camber 5.3% at 52.1% chord 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 Source UIUC Airfoil Coordinates Database
(s832-nr) NREL's S832 Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	NREL HAWT airfoil S832 Max thickness 14.9% at 44% chord Max camber 5.3% at 44% chord Source NWTC National WInd Technology Center

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