Airfoil Tools
Search 1638 airfoils

You have 0 airfoils loaded.
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.

(fx63137sm-il) FX 63-137 13.7% smoothed		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 63-137 airfoil (smoothed) Max thickness 13.7% at 30.9% chord Max camber 5.8% at 56.5% chord Max Cl/Cd 117.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx73170a-il) WORTMANN FX 73-170 A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 73-170 A airfoil Max thickness 17.1% at 43.5% chord Max camber 5.6% at 43.5% chord Max Cl/Cd 117.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe458-il) GOE 458 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 458 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 117.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e657-il) EPPLER 657 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E657 sailplane airfoil Max thickness 15.6% at 37% chord Max camber 4.6% at 47.6% chord Max Cl/Cd 117.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx83w108-il) FX 83-W-108		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 83-W-108 airfoil for use on wind turbines (W) Max thickness 10.9% at 30.9% chord Max camber 4.2% at 53.3% chord Max Cl/Cd 117.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(e377m-il) EPPLER 377 (MODIFIED) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E377 (modified) ultralight airfoil Max thickness 3.8% at 6.1% chord Max camber 9.2% at 32.6% chord Max Cl/Cd 117.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e393-il) EPPLER 393 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E393 airfoil Max thickness 11.5% at 32.3% chord Max camber 4% at 46% chord Max Cl/Cd 117.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx72150b-il) WORTMANN FX 72-MS-150B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 72-MS-150B airfoil Max thickness 15% at 37.1% chord Max camber 9.7% at 46.7% chord Max Cl/Cd 117.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e174-il) E174 (Dicke 8.92%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E174 low Reynolds number airfoil Max thickness 8.9% at 31.2% chord Max camber 3.3% at 44.9% chord Max Cl/Cd 117.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe395-il) GOE 395 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 395 airfoil Max thickness 6.1% at 19.9% chord Max camber 7% at 49.9% chord Max Cl/Cd 117.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database