Airfoil Tools
Search 1638 airfoils

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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.

(ua79sff-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP Max thickness 8.7% at 73.1% chord Max camber 3.4% at 78.1% chord Max Cl/Cd 25.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ah93w480b-il) AH 93-W-480B		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord Max Cl/Cd 24.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ys900-il) YS-900		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	YS900 hyrdofoil (Shen / Eppler) Max thickness 9% at 52.5% chord Max camber 0% at 0% chord Max Cl/Cd 24.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe570-il) GOE 570 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 570 airfoil Max thickness 33.7% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 23.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ah93w480b-il) AH 93-W-480B		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord Max Cl/Cd 23.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(hs1430-il) HAM-STD HS1-430 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	HS1 family of prop airfoils from US Patent No. 4 Max thickness 30% at 34% chord Max camber 3% at 44% chord Max Cl/Cd 23.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe570-il) GOE 570 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 570 airfoil Max thickness 33.7% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 15.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(griffith30symsuction-il) Griffith 30% Suction Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord Max Cl/Cd 15 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(chen-il) CHEN AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Illinois at Urbana-Champaign / Chen high lift airfoil Max thickness 12.5% at 27.7% chord Max camber 7.8% at 25.4% chord Max Cl/Cd 13.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(griffith30symsuction-il) Griffith 30% Suction Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord Max Cl/Cd 12.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database