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.

(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
(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
(goe15k-il) GOE 15K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 15K airfoil Max thickness 15% at 50% chord Max camber 3.4% at 50% chord Source UIUC Airfoil Coordinates Database
(goe164-il) GOE 164 (MVA MK.10) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 164 (MVA MK.10) airfoil Max thickness 8.9% at 19.9% chord Max camber 6.6% at 39.9% chord Source UIUC Airfoil Coordinates Database

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