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.

(giiim-il) GIII BL430 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Grumman/Gulfstream GIII transonic airfoils Max thickness 8.5% at 35.2% chord Max camber 1.9% at 25.2% chord Max Cl/Cd 85.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe765-il) Gottingen 765 airfoil (recovered). Thick: .144 LE radius: 0.02062 LE slope: 0.17300		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Used on the Me163 Komet Max thickness 14.4% at 30% chord Max camber 1.9% at 25.9% chord Max Cl/Cd 85.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(joukowsk0015-jf) Joukovsky f=0% t=15%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file
	Joukowski 15% symmetrical airfoil Max thickness 15% at 24.6% chord Max camber 0% at 0% chord Max Cl/Cd 85.8 at Re# 1,000,000 Source Javafoil generated
(eiffel430-il) Eiffel 430 (Lachassgne)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eiffel 430 (Lachassgne) airfoil Max thickness 9.7% at 15% chord Max camber 4.5% at 40% chord Max Cl/Cd 85.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s8038-il) S8038 (13%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S8038 (13%) low Reynolds number airfoil Max thickness 13% at 32.9% chord Max camber 0.6% at 40.1% chord Max Cl/Cd 85.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(ag38-il) AG38		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG38 airfoil Max thickness 7% at 27.7% chord Max camber 2% at 36.7% chord Max Cl/Cd 85.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx60177-il) FX 60-177 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 60-177 airfoil Max thickness 17.7% at 37.1% chord Max camber 2.7% at 77.8% chord Max Cl/Cd 85.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(b737a-il) BOEING 737 ROOT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing Commercial Airplane Company model 737 airfoils Max thickness 15.4% at 19.6% chord Max camber 0.2% at 5% chord Max Cl/Cd 85.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(naca64210-il) NACA 64-210		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 64-210 airfoil Max thickness 10% at 40% chord Max camber 1.1% at 50% chord Max Cl/Cd 85.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe165-il) GOE 165 (MVA MK.11) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 165 (MVA MK.11) airfoil Max thickness 12.1% at 19.7% chord Max camber 5.7% at 49.7% chord Max Cl/Cd 85.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database