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.

(fx60100sm-il) FX60-100 10.0% smoothed		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 60-100 airfoil (smoothed) Max thickness 10% at 27.9% chord Max camber 3.5% at 56.5% chord Max Cl/Cd 120.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx75193-il) WORTMANN FX 75-193		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 75-193 airfoil Max thickness 19.3% at 40.2% chord Max camber 3.7% at 69.1% chord Max Cl/Cd 120.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s1223-il) S1223		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S1223 high lift low Reynolds number airfoil Max thickness 12.1% at 19.8% chord Max camber 8.1% at 49% chord Max Cl/Cd 120 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe798-il) GOE 798 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 798 airfoil Max thickness 20% at 30% chord Max camber 6% at 40% chord Max Cl/Cd 120 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e197-il) E197 (13.49%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E197 low Reynolds number airfoil Max thickness 13.5% at 34.6% chord Max camber 2.8% at 43.7% chord Max Cl/Cd 119.9 at Re# 1,000,000 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 119.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e552-il) EPPLER 552 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E552 general aviation airfoil Max thickness 18.4% at 32.4% chord Max camber 2.6% at 51.8% chord Max Cl/Cd 119.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe182-il) GOE 182 (MVA H.27) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 182 (MVA H.27) airfoil Max thickness 9.5% at 19.9% chord Max camber 5.3% at 39.9% chord Max Cl/Cd 119.8 at Re# 1,000,000 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 119.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe408-il) GOE 408 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 408 airfoil Max thickness 7.8% at 30% chord Max camber 4.1% at 30% chord Max Cl/Cd 119.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database