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.

(e395-il) EPPLER 395 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E395 human e664ered aircraft airfoil Max thickness 12.3% at 29.5% chord Max camber 5.2% at 52.3% chord Max Cl/Cd 61.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe397-il) GOE 397 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 397 airfoil Max thickness 5.1% at 30% chord Max camber 4% at 40% chord Max Cl/Cd 61.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx60100-il) FX 60-100 AIRFOIL		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 Max thickness 10% at 27.9% chord Max camber 3.6% at 56.5% chord Max Cl/Cd 61.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe400-il) GOE 400 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 400 airfoil Max thickness 6.1% at 20% chord Max camber 4.9% at 40% chord Max Cl/Cd 61.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe346-il) GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 346 (Friedrichshafen-Staaken) airfoil Max thickness 5.7% at 39.9% chord Max camber 3.8% at 39.9% chord Max Cl/Cd 61.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database

(hq309-il) HQ 3.0/9 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.0/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 61.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(raf32md-il) RAF 32 MOD AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-32 MOD airfoil Max thickness 10.2% at 30% chord Max camber 4% at 50% chord Max Cl/Cd 61.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe610b-il) GOE 610 B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 610 B airfoil Max thickness 7.8% at 39.9% chord Max camber 5.3% at 39.9% chord Max Cl/Cd 61.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe301-il) GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 301 (Friedrichshafen G 13) airfoil Max thickness 10% at 28.9% chord Max camber 6.5% at 39.9% chord Max Cl/Cd 61.2 at Re# 100,000 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 61.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database