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.

(raf30-il) RAF 30 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-30 airfoil Max thickness 12.6% at 30% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(raf33-il) RAF 33 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-33 airfoil Max thickness 12.6% at 30% chord Max camber 4.7% at 30% chord Source UIUC Airfoil Coordinates Database
(raf34-il) RAF 34 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-34 airfoil Max thickness 12.6% at 30% chord Max camber 2% at 30% chord Source UIUC Airfoil Coordinates Database
(ah63k127-il) AH 63-K-127/24		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 63-K-127/24 airfoil for use with flaps (K) Max thickness 12.7% at 40.2% chord Max camber 3.8% at 43.5% chord Source UIUC Airfoil Coordinates Database
(boe103-il) BOEING 103 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing 103 airfoil Max thickness 12.7% at 30% chord Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database
(fg4-il) Fage & Collins 4		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Fage & Collins 4 airfoil Max thickness 12.7% at 30% chord Max camber 4.7% at 30% chord Source UIUC Airfoil Coordinates Database
(goe190-il) GOE 190 (MVA MK.18) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 190 (MVA MK.18) airfoil Max thickness 12.7% at 19.7% chord Max camber 5.9% at 49.7% chord Source UIUC Airfoil Coordinates Database
(goe409-il) GOE 409 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 409 airfoil Max thickness 12.7% at 30% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(goe418-il) GOE 418 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 418 airfoil Max thickness 12.7% at 20% chord Max camber 5.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe447-il) GOE 447 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 447 airfoil Max thickness 12.7% at 29.7% chord Max camber 8% at 39.7% chord Source UIUC Airfoil Coordinates Database

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