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.

(fx74130wp1-il) FX 74-130 WP1		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 74-130 WP1 airfoil Max thickness 13% at 46.7% chord Max camber 3.8% at 50% chord Max Cl/Cd 119.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e59-il) EPPLER 59 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E59 low Reynolds number airfoil Max thickness 5.6% at 25% chord Max camber 5.2% at 50% chord Max Cl/Cd 119.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx63137-il) WORTMANN FX 63-137 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil Max thickness 13.7% at 30.9% chord Max camber 6% at 53.3% chord Max Cl/Cd 119.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e49-il) EPPLER 49 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E49 low Reynolds number airfoil Max thickness 7.2% at 38.4% chord Max camber 6.5% at 62.2% chord Max Cl/Cd 119.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(hq3510-il) HQ 3.5/10 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.5/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 3.5% at 50% chord Max Cl/Cd 119 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(ys930-il) YS-930		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	YS930 hydrofoil (Shen / Eppler) Max thickness 9.1% at 35% chord Max camber 2.9% at 59.2% chord Max Cl/Cd 119 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e656-il) EPPLER 656 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E656 sailplane airfoil Max thickness 16.2% at 37% chord Max camber 4.8% at 42.2% chord Max Cl/Cd 118.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(s832-nr) NREL's S832 Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	NREL HAWT airfoil S832 Max thickness 14.9% at 44% chord Max camber 5.3% at 44% chord Max Cl/Cd 118.9 at Re# 500,000 Source NWTC National WInd Technology Center
(fx78k140a20-il) FX 78-K-140 A/20		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 78-K-140 airfoil for use with flaps (K) A/20 Max thickness 14.1% at 43.5% chord Max camber 4.4% at 43.5% chord Max Cl/Cd 118.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(davissm-il) davissm		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Davis 3R F1B free flight airfoil (smoothed) Max thickness 5.9% at 30.6% chord Max camber 5.9% at 45.4% chord Max Cl/Cd 118.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database