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.

(goe137-il) GOE 137 (MVA H.15) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 137 (MVA H.15) airfoil Max thickness 8.6% at 29.9% chord Max camber 4.4% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe13k-il) GOE 13K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 13K airfoil Max thickness 14.8% at 50% chord Max camber 5.5% at 60% chord Source UIUC Airfoil Coordinates Database
(goe14-il) GOE 14 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 14 airfoil Max thickness 9.9% at 29.8% chord Max camber 6.9% at 29.8% chord Source UIUC Airfoil Coordinates Database
(goe140-il) GOE 140 (MVA H.17) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 140 (MVA H.17) airfoil Max thickness 8.8% at 29.9% chord Max camber 5.3% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe142-il) GOE 142 (MVA H.19) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 142 (MVA H.19) airfoil Max thickness 6.2% at 24.9% chord Max camber 3.8% at 34.9% chord Source UIUC Airfoil Coordinates Database
(goe143-il) GOE 143 (MVA H.20) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 143 (MVA H.20) airfoil Max thickness 7.4% at 19.9% chord Max camber 3.8% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe144-il) GOE 144 (MVA H.21) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 144 (MVA H.21) airfoil Max thickness 7.3% at 19.9% chord Max camber 4.7% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe147-il) GOE 147 (MVA H.6) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 147 (MVA H.6) airfoil Max thickness 7.5% at 14.9% chord Max camber 3.8% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe14k-il) GOE 14K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 14K airfoil Max thickness 12% at 50% chord Max camber 2.7% at 50% chord Source UIUC Airfoil Coordinates Database
(goe15-il) GOE 15 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 15 airfoil Max thickness 9% at 29.8% chord Max camber 7.8% at 29.8% chord Source UIUC Airfoil Coordinates Database

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