Airfoil Tools
Search 1638 airfoils

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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.

(e226-il) E226 (10.19%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E226 low Reynolds number airfoil Max thickness 10.2% at 31.3% chord Max camber 0.5% at 56.9% chord Max Cl/Cd 67.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(joukowsk0018-jf) Joukovsky f=0% t=18%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file
	Joukowski 18% symmetrical airfoil Max thickness 18% at 27.1% chord Max camber 0% at 0% chord Max Cl/Cd 67.2 at Re# 500,000 Source Javafoil generated
(p51hroot-il) NACA 66		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 66 Max thickness 15.5% at 45% chord Max camber 1.3% at 47.5% chord Max Cl/Cd 67.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(s4095-il) S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane. Max thickness 9.7% at 29.1% chord Max camber 1.7% at 33.7% chord Max Cl/Cd 67.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(eh1070-il) Eh 1.0/7.0		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	John Yost EH 1.0/7.0 for tailless R/C aircraft Max thickness 7% at 28.7% chord Max camber 1% at 25.9% chord Max Cl/Cd 67.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(e904-il) EPPLER 904 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E904 hydrofoil Max thickness 9% at 44.9% chord Max camber 1.3% at 50.4% chord Max Cl/Cd 67.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(p51htip-il) NACA 66		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 66 Max thickness 12% at 45% chord Max camber 1.3% at 47.5% chord Max Cl/Cd 67 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(sc20706-il) NASA SC(2)-0706 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NASA SC(2)-0706 airfoil (NASA TP-2969) Max thickness 6% at 34% chord Max camber 1.6% at 82% chord Max Cl/Cd 67 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe703-il) GOE 703 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 703 airfoil Max thickness 19.4% at 30% chord Max camber 2.3% at 30% chord Max Cl/Cd 67 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe511-il) GOE 511 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 511 airfoil Max thickness 16.6% at 19.9% chord Max camber 8% at 29.8% chord Max Cl/Cd 67 at Re# 500,000 Source UIUC Airfoil Coordinates Database