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.

(goe332-il) GOE 332 (PFALZ 61) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 332 (Pfalz 61) airfoil Max thickness 11.8% at 29.8% chord Max camber 6.4% at 39.8% chord Max Cl/Cd 120.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe450-il) GOE 450 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 450 airfoil Max thickness 8.9% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 120.7 at Re# 500,000 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 120.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e392-il) E392 (10.15%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E392 low Reynolds number airfoil Max thickness 10.1% at 31.6% chord Max camber 3.7% at 45.3% chord Max Cl/Cd 120.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe547-il) GOE 547 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 547 airfoil Max thickness 10.5% at 29.7% chord Max camber 4% at 49.7% chord Max Cl/Cd 120.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(e64-il) E64 (8.45%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E64 low Reynolds number airfoil Max thickness 8.4% at 27.8% chord Max camber 2.9% at 56.5% chord Max Cl/Cd 120.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e423-il) E423		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E423 high lift airfoil Max thickness 12.5% at 23.7% chord Max camber 9.5% at 41.4% chord Max Cl/Cd 120.6 at Re# 500,000 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 120.5 at Re# 500,000 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 120.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(usa98-il) USA 98 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-98 airfoil Max thickness 14.3% at 30% chord Max camber 6.4% at 50% chord Max Cl/Cd 120.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database