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.

(fx84w127-il) FX 84-W-127		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-127 airfoil for use on wind turbines (W) Max thickness 12.8% at 33.9% chord Max camber 3.7% at 40.2% chord Max Cl/Cd 142.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe592-il) GOE 592 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 592 airfoil Max thickness 14.3% at 29.7% chord Max camber 7.5% at 39.7% chord Max Cl/Cd 142.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e399-il) EPPLER 399 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E399 human powered aircraft airfoil Max thickness 14.8% at 29% chord Max camber 5.1% at 51.4% chord Max Cl/Cd 142.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe425-il) GOE 425 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 425 airfoil Max thickness 16% at 29.3% chord Max camber 4.5% at 39.3% chord Max Cl/Cd 142.1 at Re# 1,000,000 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 142 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(goe426-il) GOE 426 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 426 airfoil Max thickness 13.6% at 30% chord Max camber 4.6% at 40% chord Max Cl/Cd 141.9 at Re# 1,000,000 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 141.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e376-il) EPPLER 376 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E376 ultralight airfoil Max thickness 2.5% at 4.3% chord Max camber 9% at 32.7% chord Max Cl/Cd 141.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe396-il) GOE 396 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 396 airfoil Max thickness 4.7% at 30% chord Max camber 5.8% at 40% chord Max Cl/Cd 141.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(strand-il) STRAND AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Strand high lift airfoil Max thickness 15.4% at 26.1% chord Max camber 4.1% at 32.1% chord Max Cl/Cd 141.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database