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.

(goe547-il) GOE 547 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 547 airfoil Max thickness 10.5% at 29.7% chord Max camber 4% at 49.7% chord Max Cl/Cd 143.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx78k150-il) FX 78-K-150/20		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 78-K-150/20 airfoil for use with flaps (K) Max thickness 15.1% at 43.5% chord Max camber 4.3% at 43.5% chord Max Cl/Cd 143.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e583-il) EPPLER 583 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E583 sailplane airfoil Max thickness 16.5% at 38% chord Max camber 4.5% at 38% chord Max Cl/Cd 143.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe08k-il) GOE 8K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 8K airfoil Max thickness 14.9% at 50% chord Max camber 6.1% at 50% chord Max Cl/Cd 143.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(sa7026-il) SA7026		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig / Ashok Gopalarathnam SA7026 low Reynolds number airfoil Max thickness 9% at 32.9% chord Max camber 3.8% at 47.1% chord Max Cl/Cd 143.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(fx78k140a20-il) FX 78-K-140 A/20		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 78-K-140 airfoil for use with flaps (K) A/20 Max thickness 14.1% at 43.5% chord Max camber 4.4% at 43.5% chord Max Cl/Cd 142.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe07k-il) GOE 7K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 7K airfoil Max thickness 11% at 50% chord Max camber 4.5% at 50% chord Max Cl/Cd 142.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(stf86361-il) EPPLER STF 863-615 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler STF 863-615 airfoil Max thickness 14.7% at 44.7% chord Max camber 4.2% at 72.3% chord Max Cl/Cd 142.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(naca6412-il) NACA 6412		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 6412 airfoil Max thickness 12% at 30.1% chord Max camber 6% at 39.6% chord Max Cl/Cd 142.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e377m-il) EPPLER 377 (MODIFIED) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E377 (modified) ultralight airfoil Max thickness 3.8% at 6.1% chord Max camber 9.2% at 32.6% chord Max Cl/Cd 142.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database