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.

(goe526-il) GOE 526 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 526 airfoil Max thickness 12.3% at 29.7% chord Max camber 4.1% at 39.7% chord Max Cl/Cd 107.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe413-il) GOE 413 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 413 airfoil Max thickness 16.4% at 30% chord Max camber 4.6% at 40% chord Max Cl/Cd 107.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(nlf415-il) NASA/LANGLEY NLF(2)-0415 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NASA/Langley-DFVLR/Somers(NASA)-Horstmann(DFVLR) NLF(2)-0415 natural laminar flow airfoil Max thickness 15% at 47.1% chord Max camber 3% at 71.4% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(hq2511-il) HQ 2.5/11 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 2.5/11 R/C sailplane airfoil Max thickness 11% at 33.9% chord Max camber 2.5% at 50% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(sd7080-il) SD7080 (9.2%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD7080 low Reynolds number airfoil Max thickness 9.2% at 30% chord Max camber 2.1% at 44.4% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(e1212-il) EPPLER E1212 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E1212 general aviation airfoil Max thickness 17.7% at 23.4% chord Max camber 3.2% at 36.4% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(clarkw-il) CLARK W AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	CLARK W airfoil Max thickness 11.2% at 30% chord Max camber 3.7% at 40% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(mh18-il) MH 18 11.16%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 18 for F3D Pylon Racing Max thickness 11.1% at 36.8% chord Max camber 2.7% at 42.1% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(rg8-il) RG 8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Rolf Girsberger RG 8 airfoil Max thickness 10.8% at 31.1% chord Max camber 2.2% at 60.5% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(naca4418-il) NACA 4418		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 4418 airfoil Max thickness 18% at 30% chord Max camber 4% at 40% chord Max Cl/Cd 107.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database