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.

(fx6617ai-il) WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-17AII-182 airfoil (as tested at NASA) Max thickness 18.8% at 35.3% chord Max camber 3.7% at 40.2% chord Max Cl/Cd 6.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(n6h20-il) NACA 6-H-20 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 6-H-20 rotorcraft airfoil Max thickness 20% at 40% chord Max camber 6.1% at 40% chord Max Cl/Cd 6 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx66182-il) FX 66-182 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-182 airfoil Max thickness 18.2% at 33.9% chord Max camber 3.8% at 37.1% chord Max Cl/Cd 5.9 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx6617a2-il) FX 66-17AII-182 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-17AII-182 airfoil Max thickness 18.2% at 33.9% chord Max camber 3.8% at 37.1% chord Max Cl/Cd 5.9 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx66196v-il) FX 66-S-196 V1 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-S-196 V1 airfoil Max thickness 19.6% at 37.1% chord Max camber 4% at 46.7% chord Max Cl/Cd 5.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database

(jn153-il) JN-153 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Narramore JN153 airfoil Max thickness 17.6% at 28.2% chord Max camber 8.4% at 38.1% chord Max Cl/Cd 5.6 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx79w660a-il) FX 79-W-660A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortman FX 79-W-660A airfoil for use on wind turbines (W) Max thickness 66.4% at 46.7% chord Max camber 2.3% at 17% chord Max Cl/Cd 5.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx79w660a-il) FX 79-W-660A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortman FX 79-W-660A airfoil for use on wind turbines (W) Max thickness 66.4% at 46.7% chord Max camber 2.3% at 17% chord Max Cl/Cd 5.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(e862-il) EPPLER 862 STRUT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E862 strut airfoil Max thickness 32.4% at 28.5% chord Max camber 0% at 0% chord Max Cl/Cd 5.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx08s176-il) WORTMANN FX 08-S-176 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 08-S-176 airfoil Max thickness 17.6% at 37.1% chord Max camber 5.7% at 37.1% chord Max Cl/Cd 5.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database