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.

(la203a-il) DOUGLAS LA203A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Douglas/Liebeck LA203A high lift airfoil Max thickness 15.7% at 34.3% chord Max camber 5.5% at 46% chord Max Cl/Cd 160.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(hs1606-il) HAM-STD HS1-606 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	HS1 family of prop airfoils from US Patent No. 4 Max thickness 6% at 18% chord Max camber 4.4% at 46% chord Max Cl/Cd 160.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx72150a-il) WORTMANN FX 72-MS-150A 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-150A airfoil Max thickness 15% at 37.1% chord Max camber 8.3% at 46.7% chord Max Cl/Cd 160.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e385-il) E385 (8.41%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E385 airfoil Max thickness 8.4% at 29.6% chord Max camber 5.3% at 47.5% chord Max Cl/Cd 159.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe07k-il) GOE 7K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 7K airfoil Max thickness 11% at 50% chord Max camber 4.5% at 50% chord Max Cl/Cd 159.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(goe500-il) GOE 500 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 500 airfoil Max thickness 10% at 30% chord Max camber 6% at 50% chord Max Cl/Cd 159.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe495-il) GOE 495 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 495 airfoil Max thickness 6.9% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 158.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(mh115-il) MH 115 11.06%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 115 for a propeller for ultralight Max thickness 11.1% at 29.8% chord Max camber 5.5% at 46% chord Max Cl/Cd 158.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx74cl6140-il) FX 74-CL6-140		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 74-CL6-140 airfoil Max thickness 14.1% at 30.9% chord Max camber 7.1% at 33.9% chord Max Cl/Cd 158.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e654-il) EPPLER 654 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E654 sailplane airfoil Max thickness 17.2% at 36.1% chord Max camber 4.9% at 46.5% chord Max Cl/Cd 158.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database