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.

(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 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe692-il) GOE 692 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 692 airfoil Max thickness 16.1% at 30% chord Max camber 5% at 40% chord Max Cl/Cd 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(rg8-il) RG 8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Rolf Girsberger RG 8 airfoil Max thickness 10.8% at 31.1% chord Max camber 2.2% at 60.5% chord Max Cl/Cd 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx77w121-il) FX 77-W-121		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 77-W-121 airfoil for use on wind turbines (W) Max thickness 12.1% at 30.9% chord Max camber 4.6% at 30.9% chord Max Cl/Cd 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe176-il) GOE 176 (ALBATROS 7020) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 176 (Albatros 7020) airfoil Max thickness 10.3% at 19.8% chord Max camber 5.6% at 39.8% chord Max Cl/Cd 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(goe315-il) GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 315 (Hansa-Brandenburg III.5) airfoil Max thickness 8.1% at 29.9% chord Max camber 4.1% at 29.9% chord Max Cl/Cd 73.6 at Re# 200,000 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 73.6 at Re# 200,000 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 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe457-il) GOE 457 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 457 airfoil Max thickness 7.8% at 19.9% chord Max camber 4.2% at 39.9% chord Max Cl/Cd 73.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe532-il) GOE 532 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 532 airfoil Max thickness 12.5% at 30% chord Max camber 4.8% at 40% chord Max Cl/Cd 73.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database