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.

(e193-il) E193 (10.22%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E193 low Reynolds number airfoil Max thickness 10.2% at 31% chord Max camber 3% at 44.7% chord Max Cl/Cd 58.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe331-il) GOE 331 (PFALZ 60) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 331 (Pfalz 60) airfoil Max thickness 10.6% at 29.9% chord Max camber 6.9% at 39.9% chord Max Cl/Cd 58.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe167-il) GOE 167 (V.KARMAN PROP.2) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 167 (V.Karman PROP.2) airfoil Max thickness 10.1% at 29.9% chord Max camber 4.5% at 29.9% chord Max Cl/Cd 58.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe391-il) GOE 391 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 391 airfoil Max thickness 5.1% at 40% chord Max camber 3.2% at 40% chord Max Cl/Cd 58.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(s4180-il) S4180-098-84		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S4180 low Reynolds number airfoil Max thickness 9.8% at 26.1% chord Max camber 4% at 39.4% chord Max Cl/Cd 58.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database

(e212-il) E212 (10.55%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E212 low Reynolds number airfoil Max thickness 10.6% at 27.5% chord Max camber 2.5% at 61.3% chord Max Cl/Cd 58.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(s3025-il) S3025 9.38%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S3025 low Reynolds number airfoil Max thickness 9.4% at 30.9% chord Max camber 3% at 44.9% chord Max Cl/Cd 58.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(naca6412-il) NACA 6412		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 6412 airfoil Max thickness 12% at 30.1% chord Max camber 6% at 39.6% chord Max Cl/Cd 58.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe101-il) GOE 101 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 101 airfoil Max thickness 6.9% at 30% chord Max camber 4% at 30% chord Max Cl/Cd 58.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe376-il) GOE 376 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 376 airfoil Max thickness 6.6% at 30% chord Max camber 5% at 30% chord Max Cl/Cd 58.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database