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.

(isa962-il) I.S.A. 962		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	I.S.A. 962 airfoil Max thickness 9.6% at 20% chord Max camber 4.6% at 40% chord Max Cl/Cd 77.1 at Re# 200,000 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 77 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(s4233-il) S4233-136-84		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S4233 low Reynolds number airfoil Max thickness 13.6% at 34.9% chord Max camber 2.7% at 48.8% chord Max Cl/Cd 77 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe06k-il) GOE 6K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 6K airfoil Max thickness 7.5% at 50% chord Max camber 3.1% at 50% chord Max Cl/Cd 77 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(mh117-il) MH 117 9.8%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 117 for a propeller for ultralight (tip) Max thickness 9.8% at 29.1% chord Max camber 2.7% at 44.6% chord Max Cl/Cd 77 at Re# 200,000 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 76.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe591-il) GOE 591 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 591 airfoil Max thickness 11.2% at 30% chord Max camber 5.1% at 40% chord Max Cl/Cd 76.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx84w097-il) FX 84-W-097		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-097 airfoil for use on wind turbines (W) Max thickness 9.7% at 33.9% chord Max camber 2.8% at 37.1% chord Max Cl/Cd 76.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(hq2512-il) HQ 2.5/12 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 2.5/12 R/C sailplane airfoil Max thickness 12% at 35% chord Max camber 2.5% at 50% chord Max Cl/Cd 76.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe399-il) GOE 399 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 399 airfoil Max thickness 6.9% at 29.9% chord Max camber 4.2% at 39.9% chord Max Cl/Cd 76.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database