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.

(gs1-il) SIKORSKY GS-1 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gluharoff/Sikorsky GS-1 airfoil Max thickness 13.9% at 30% chord Max camber 4.1% at 50% chord Max Cl/Cd 119.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s3021-il) S3021-095-84		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S3021 low Reynolds number airfoil Max thickness 9.5% at 30% chord Max camber 2.5% at 39.2% chord Max Cl/Cd 119.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(ah21-7-il) AH21 7% version (Andrew Hollom)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Andrew Hollom AH 21 airfoil (7% version) Max thickness 9% at 34.9% chord Max camber 2.3% at 54.8% chord Max Cl/Cd 119.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe389-il) GOE 389 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 389 airfoil Max thickness 10.3% at 29.8% chord Max camber 4% at 39.8% chord Max Cl/Cd 119.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(cr001sm-il) cr001sm		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Cody Robertson CR 001 R/C hand-launch low Reynolds number airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 4.1% at 45.4% chord Max Cl/Cd 119.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(sd6080-il) SD6080 (9.2%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD6080 low Reynolds number airfoil Max thickness 9.2% at 30.9% chord Max camber 3.2% at 44.7% chord Max Cl/Cd 119.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe140-il) GOE 140 (MVA H.17) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 140 (MVA H.17) airfoil Max thickness 8.8% at 29.9% chord Max camber 5.3% at 29.9% chord Max Cl/Cd 119.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e176-il) E176 (8.83%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E176 low Reynolds number airfoil Max thickness 8.8% at 30.5% chord Max camber 2.9% at 44.2% chord Max Cl/Cd 119.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(clarkysm-il) CLARK-Y 11.7% smoothed		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	CLARK Y airfoil (smoothed) Max thickness 11.7% at 30.9% chord Max camber 3.5% at 43.5% chord Max Cl/Cd 119.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe361-il) GOE 361 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 361 airfoil Max thickness 6.8% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 119.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database