Airfoil Tools
Search 1638 airfoils

You have 0 airfoils loaded.
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.

(ah94145-il) AH 94-145		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 94-145 airfoil Max thickness 14.6% at 38.9% chord Max camber 5.6% at 44.6% chord Max Cl/Cd 135.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe494-il) GOE 494 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 494 airfoil Max thickness 5% at 20% chord Max camber 5.1% at 50% chord Max Cl/Cd 135.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ch10sm-il) CH10 (smoothed)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Chuch Hollinger CH 10-48-13 high lift low Reynolds number airfoil Max thickness 12.8% at 30.6% chord Max camber 10.2% at 49.3% chord Max Cl/Cd 135.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e396-il) EPPLER 396 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E396 human powered aircraft airfoil Max thickness 13.1% at 29.5% chord Max camber 5.4% at 52.1% chord Max Cl/Cd 135.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e376-il) EPPLER 376 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E376 ultralight airfoil Max thickness 2.5% at 4.3% chord Max camber 9% at 32.7% chord Max Cl/Cd 135 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(fx74080-il) WORTMANN FX 74-080		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 74-080 airfoil Max thickness 8.2% at 43.5% chord Max camber 4.3% at 46.7% chord Max Cl/Cd 134.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e377-il) EPPLER 377 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E377 ultralight airfoil Max thickness 3.9% at 8.4% chord Max camber 8.8% at 36.9% chord Max Cl/Cd 133.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(hs1606-il) HAM-STD HS1-606 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 6% at 18% chord Max camber 4.4% at 46% chord Max Cl/Cd 133.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e385-il) E385 (8.41%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E385 airfoil Max thickness 8.4% at 29.6% chord Max camber 5.3% at 47.5% chord Max Cl/Cd 133.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe495-il) GOE 495 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 495 airfoil Max thickness 6.9% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 132.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database