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.

(mrc-20-il) MRC-20		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela MRC-20 Max thickness 15.6% at 38.2% chord Max camber 2.9% at 48% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe222-il) GOE 222 (MVA H.33) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 222 (MVA H.33) airfoil Max thickness 18.5% at 29.2% chord Max camber 7.2% at 49.2% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx61147-il) FX 61-147 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 61-147 airfoil Max thickness 14.8% at 33.9% chord Max camber 3.2% at 33.9% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ah82150f-il) AH 82-150 F		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 82-150 F airfoil Max thickness 15% at 43.5% chord Max camber 3.6% at 46.7% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe692-il) GOE 692 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 692 airfoil Max thickness 16.1% at 30% chord Max camber 5% at 40% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(goe630-il) GOE 630 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 630 airfoil Max thickness 12.6% at 29.8% chord Max camber 7.7% at 39.8% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe180-il) GOE 180 (MVA H.26) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 180 (MVA H.26) airfoil Max thickness 8.7% at 30% chord Max camber 4.4% at 40% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe133-il) GOE 133 (MVA H.11) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 133 (MVA H.11) airfoil Max thickness 7.9% at 30% chord Max camber 4.3% at 30% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(naca633418-il) NACA 63		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 63 Max thickness 18% at 33.9% chord Max camber 2.2% at 50% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe358-il) GOE 358 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 358 airfoil Max thickness 10.9% at 20% chord Max camber 5.6% at 50% chord Max Cl/Cd 99.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database