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.

(lg10sc-il) LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Lockheed-Georgia/NASA/Blackwell rotorcraft airfoil Max thickness 10% at 32% chord Max camber 1.5% at 16% chord Max Cl/Cd 90.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(pw51-pw) PW51		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	Peter Wick. Airfoil for plank model gliders Max thickness 8.9% at 27.5% chord Max camber 1.4% at 27.5% chord Max Cl/Cd 90.8 at Re# 1,000,000 Source RC Groups
(as5046-il) AS5046 (16%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	AS5046 airfoil Ashok Gopalarathnam/Selig 16% airfoil Max thickness 16% at 37.6% chord Max camber 0.7% at 77.4% chord Max Cl/Cd 90.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e326-il) EPPLER 326 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E326 flying wing airfoil Max thickness 12.9% at 33.4% chord Max camber 2.1% at 19.5% chord Max Cl/Cd 90.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e186-il) E186 (10.27%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E186 low Reynolds number airfoil Max thickness 10.2% at 29% chord Max camber 0.8% at 29% chord Max Cl/Cd 90.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(sc1012r8-il) SIKORSKY SC1012R8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Sikorsky SC1012 R8 rotorcraft airfoil Max thickness 12% at 27.8% chord Max camber 2.7% at 21.8% chord Max Cl/Cd 90.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(isa961-il) I.S.A. 961		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	I.S.A. 961 airfoil Max thickness 9.3% at 20% chord Max camber 4.6% at 40% chord Max Cl/Cd 90.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e502-il) EPPLER 502 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E502 general purpose airfoil Max thickness 15.6% at 42.1% chord Max camber 1.5% at 32.3% chord Max Cl/Cd 90.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(nacam6-il) NACA M6		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA M6 airfoil Max thickness 12% at 30% chord Max camber 2.1% at 30% chord Max Cl/Cd 90.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx84w218-il) FX 84-W-218		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-218 airfoil for use on wind turbines (W) Max thickness 22% at 33.9% chord Max camber 3.2% at 43.5% chord Max Cl/Cd 90.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database