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.

(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 39.6 at Re# 50,000 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 39.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(ag27-il) AG27 Bubble Dancer DLG by Mark Drela		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG27 airfoil used on the Bubble Dancer R/C DLG Max thickness 6.1% at 21.7% chord Max camber 2.6% at 44% chord Max Cl/Cd 39.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(hq259-il) HQ 2.5/9 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 2.5/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 2.5% at 50% chord Max Cl/Cd 39.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe379-il) GOE 379 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 379 airfoil Max thickness 6.5% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 39.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(goe328-il) GOE 328 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 328 airfoil Max thickness 8.2% at 30% chord Max camber 4.3% at 30% chord Max Cl/Cd 39.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe184-il) GOE 184 (MVA H.29) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 184 (MVA H.29) airfoil Max thickness 8.3% at 19.9% chord Max camber 5.3% at 39.9% chord Max Cl/Cd 39.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe303-il) GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 303 (Friedrichshafen G03) airfoil Max thickness 9.8% at 29.9% chord Max camber 5.9% at 39.9% chord Max Cl/Cd 39.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(hq2590sm-il) HQ 2.5/9.0 smoothed by Eppler		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 2.5/9 R/C sailplane airfoil (smoothed) Max thickness 9% at 35% chord Max camber 2.5% at 55% chord Max Cl/Cd 39.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(hq259b-il) HQ 2.5/9 B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 2.5/9 B R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 2.5% at 55% chord Max Cl/Cd 39.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database