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.

(e854-il) EPPLER E854 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E854 propeller airfoil Max thickness 13.4% at 32.3% chord Max camber 3.3% at 55.7% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(c141e-il) LOCKHEED C-141 BL761.11 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Lockheed-Georgia C-141 transonic wing airfoils Max thickness 10.5% at 40.2% chord Max camber 1.8% at 50% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe650-il) GOE 650 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 650 airfoil Max thickness 13.4% at 19.5% chord Max camber 4.4% at 49.5% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe187-il) GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 187 (Schatte-Lanz 2U10) airfoil Max thickness 8.3% at 30% chord Max camber 4.8% at 30% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e195-il) E195 (11.82%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E195 low Reynolds number airfoil Max thickness 11.8% at 35% chord Max camber 2.7% at 44.2% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(s8065-il) S8065 (11% version of S8064)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig airfoil for Q-40 pylon racing (11%). Max thickness 11% at 37.8% chord Max camber 1.1% at 56.3% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e220-il) E220 (11.48%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E220 low Reynolds number airfoil Max thickness 11.5% at 33.1% chord Max camber 2.2% at 37.7% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(giiil-il) GIII BL387 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Grumman/Gulfstream GIII transonic airfoils Max thickness 8.5% at 35.1% chord Max camber 1.6% at 25.1% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(nacam12-il) NACA M12		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA M12 airfoil Max thickness 11.9% at 30% chord Max camber 2% at 30% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(arad13-il) ARA-D 13% AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Aeronautical Research Association/Bocci-Dowty Rotol ARA-D 13% thick propeller airfoil Max thickness 13% at 25% chord Max camber 3.6% at 30% chord Max Cl/Cd 31.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database