Airfoil Tools
Search 1638 airfoils

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Your Reynold number range is 50,000 to 1,000,000. (set)

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.

(goe803h-il) GOE 803 (HACKLINGER) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 803 (Hacklinger) airfoil Max thickness 6.3% at 15% chord Max camber 6.6% at 40% chord Max Cl/Cd 40 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(fx63120-il) FX 63-120 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 63-120 airfoil Max thickness 12% at 30.8% chord Max camber 5.2% at 50% chord Max Cl/Cd 40 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe326-il) GOE 326 (PFALZ 55) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 326 (Pfalz 55) airfoil Max thickness 8.2% at 29.9% chord Max camber 4.7% at 39.9% chord Max Cl/Cd 40 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(sg6042-il) SG6042		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig / Giguere SG6042 wind turbine airfoil (high L/D) Max thickness 10% at 33.5% chord Max camber 3.3% at 51.5% chord Max Cl/Cd 40 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe174-il) GOE 174 (ALBATROS 5020) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 174 (Albatros 5020) airfoil Max thickness 8.6% at 19.9% chord Max camber 5.6% at 39.9% chord Max Cl/Cd 40 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(goe165-il) GOE 165 (MVA MK.11) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 165 (MVA MK.11) airfoil Max thickness 12.1% at 19.7% chord Max camber 5.7% at 49.7% chord Max Cl/Cd 39.9 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(sd7032-il) SD7032-099-88		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD7032 low Reynolds number airfoil Max thickness 10% at 26.6% chord Max camber 3.4% at 45.1% chord Max Cl/Cd 39.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e214-il) E214 (11.1%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E214 low Reynolds number airfoil Max thickness 11.1% at 33.1% chord Max camber 3.7% at 56.9% chord Max Cl/Cd 39.8 at Re# 50,000 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 Max Cl/Cd 39.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe257-il) GOE 257 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 257 airfoil Max thickness 8.8% at 30% chord Max camber 4.1% at 30% chord Max Cl/Cd 39.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database