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.

(fx74cl5140-il) FX74_CL5_140		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 74-CL5-140 high lift airfoil Max thickness 14% at 30.9% chord Max camber 9.9% at 37.1% chord Max Cl/Cd 118.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx74modsm-il) FX 74-Cl5-140 MOD (smoothed)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Modified Wortmann FX 74-CL5-140 high lift airfoil Max thickness 13.1% at 27.1% chord Max camber 9.7% at 41.6% chord Max Cl/Cd 118.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx72150b-il) WORTMANN FX 72-MS-150B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 72-MS-150B airfoil Max thickness 15% at 37.1% chord Max camber 9.7% at 46.7% chord Max Cl/Cd 117.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx72150b-il) WORTMANN FX 72-MS-150B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 72-MS-150B airfoil Max thickness 15% at 37.1% chord Max camber 9.7% at 46.7% chord Max Cl/Cd 117.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx74cl5140-il) FX74_CL5_140		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 74-CL5-140 high lift airfoil Max thickness 14% at 30.9% chord Max camber 9.9% at 37.1% chord Max Cl/Cd 115.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe652-il) GOE 652 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 652 airfoil Max thickness 17.1% at 20% chord Max camber 9.3% at 50% chord Max Cl/Cd 112.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(jn153-il) JN-153 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Narramore JN153 airfoil Max thickness 17.6% at 28.2% chord Max camber 8.4% at 38.1% chord Max Cl/Cd 112.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe234-il) GOE 234 (MVA CA5) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 234 (MVA CA5) airfoil Max thickness 14.2% at 19.7% chord Max camber 9.2% at 49.7% chord Max Cl/Cd 110.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e421-il) EPPLER 421 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E421 high lift airfoil Max thickness 14.5% at 26% chord Max camber 8.6% at 37.4% chord Max Cl/Cd 109.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe226-il) GOE 226 (MVA H.36) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 226 (MVA H.36) airfoil Max thickness 13.9% at 19.7% chord Max camber 8.1% at 49.7% chord Max Cl/Cd 109.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database

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