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.

(goe387-il) GOE 387 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 387 airfoil Max thickness 14.9% at 30% chord Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe493-il) GOE 493 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 493 airfoil Max thickness 14.9% at 29.3% chord Max camber 3.4% at 49.3% chord Source UIUC Airfoil Coordinates Database
(goe675-il) GOE 675 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 675 airfoil Max thickness 14.9% at 29.5% chord Max camber 5.9% at 39.5% chord Source UIUC Airfoil Coordinates Database
(goe711-il) GOE 711 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 711 airfoil Max thickness 14.9% at 30% chord Max camber 6.3% at 30% 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
(usa48-il) USA 48 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-48 airfoil Max thickness 14.9% at 30% chord Max camber 2.9% at 40% chord Source UIUC Airfoil Coordinates Database
(ah82150a-il) AH 82-150 A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 82-150 A airfoil Max thickness 15% at 40.2% chord Max camber 3.3% at 43.5% chord Source UIUC Airfoil Coordinates Database
(ah82150f-il) AH 82-150 F		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 82-150 F airfoil Max thickness 15% at 43.5% chord Max camber 3.6% at 46.7% chord Source UIUC Airfoil Coordinates Database
(ah83150q-il) AH 83-150 Q		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 83-150 Q airfoil Max thickness 15% at 40.2% chord Max camber 4.1% at 37.1% chord Source UIUC Airfoil Coordinates Database
(as5045-il) AS5045 (15%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	AS5045 airfoil Ashok Gopalarathnam/Selig 15% airfoil Max thickness 15% at 37.5% chord Max camber 1% at 27.2% chord Source UIUC Airfoil Coordinates Database

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