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.

(mue139-il) MUE 139		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	MUE 139 airfoil Max thickness 13.9% at 22.2% chord Max camber 4.7% at 30.9% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(n63010a-il) NACA 63A010 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 63-010A airfoil Max thickness 10% at 35% chord Max camber 0% at 0% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(hq010-il) HQ 0/10 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 0/10 R/C sailplane airfoil Max thickness 10% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(fx711530-il) FX 71-L-150/30 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 71-L-150/30 airfoil Max thickness 15% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(fx71l150-il) FX 71-L-150/30 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 71-L-150/30 airfoil Max thickness 15% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(mh94-il) MH 94 16.03%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 94 parafoil Max thickness 16% at 34.1% chord Max camber 1.3% at 74.1% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e327-il) EPPLER 327 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E327 flying wing airfoil Max thickness 13.1% at 32.4% chord Max camber 2.6% at 23% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(hq09-il) HQ 0/9 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 0/9 R/C sailplane airfoil Max thickness 8.1% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e851-il) EPPLER E851 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E851 propeller airfoil Max thickness 9% at 37% chord Max camber 2.3% at 66.3% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe12k-il) GOE 12K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 12K airfoil Max thickness 11.1% at 50% chord Max camber 4.1% at 60% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database