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.

(lnv109a-il) LNV109A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Douglas/Liebeck LNV109A high lift airfoil Max thickness 13% at 23.5% chord Max camber 6% at 31.5% chord Max Cl/Cd 113.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e817-il) EPPLER 817 HYDROFOIL AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E817 hydrofoil Max thickness 11% at 32.9% chord Max camber 2.9% at 66.7% chord Max Cl/Cd 113.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(l7769-il) LISSAMAN 7769 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Lissaman 7769 human powered aircraft airfoil Max thickness 11% at 30% chord Max camber 4.4% at 30% chord Max Cl/Cd 113.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ah88k130-il) AH 88-K-130/20		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 88-K-130/20 airfoil for use with flaps (K) Max thickness 13% at 43.5% chord Max camber 3.9% at 46.7% chord Max Cl/Cd 113.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(s802-nr) NREL's S802 Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	NREL HAWT airfoil S802 tip Not recommended Max thickness 11.5% at 37.9% chord Max camber 3.8% at 47.3% chord Max Cl/Cd 113.6 at Re# 500,000 Source NWTC National WInd Technology Center

(ah93w174-il) AH 93-W-174		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-174 airfoil for use on wind turbines (W) Max thickness 17.4% at 33.9% chord Max camber 3.9% at 37.1% chord Max Cl/Cd 113.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(hq3010-il) HQ 3.0/10 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.0/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 113.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(mh116-il) MH 116 9.84%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 116 for a propeller for ultralight Max thickness 9.9% at 32.4% chord Max camber 4.1% at 46.4% chord Max Cl/Cd 113.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e392-il) E392 (10.15%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E392 low Reynolds number airfoil Max thickness 10.1% at 31.6% chord Max camber 3.7% at 45.3% chord Max Cl/Cd 113.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(hq17-il) HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Airfoil measured from an ASW22 wing Max thickness 15.2% at 42% chord Max camber 4.5% at 42% chord Max Cl/Cd 113.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database