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.

(usa46-il) USA 46 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-46 airfoil Max thickness 6.5% at 20% chord Max camber 2.2% at 40% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(hs1712-il) HAM-STD HS1-712 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 12% at 36% chord Max camber 4.9% at 44% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(sd2083-il) SD2083 (9.0%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD2083 low Reynolds number airfoil Max thickness 9% at 35.2% chord Max camber 2.5% at 49.6% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(n9-il) N-9		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-9 airfoil Max thickness 8.5% at 30% chord Max camber 2.7% at 40% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e378-il) EPPLER 378 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E378 ultralight airfoil Max thickness 4.1% at 7.8% chord Max camber 8.1% at 35.9% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(goe474-il) GOE 474 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 474 airfoil Max thickness 7% at 30% chord Max camber 2.9% at 40% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(usa46-il) USA 46 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-46 airfoil Max thickness 6.5% at 20% chord Max camber 2.2% at 40% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e377-il) EPPLER 377 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E377 ultralight airfoil Max thickness 3.9% at 8.4% chord Max camber 8.8% at 36.9% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(eiffel428-il) Eiffel 428 (Bleriot)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eiffel 428 (Bleriot) airfoil Max thickness 9% at 30% chord Max camber 4.2% at 40% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe134-il) GOE 134 (MVA H.12) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 134 (MVA H.12) airfoil Max thickness 9.5% at 30% chord Max camber 4% at 30% chord Max Cl/Cd 38.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database