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.

(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 86.2 at Re# 200,000 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 86.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe304-il) GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 304 (Friedrichshafen G02) airfoil Max thickness 9% at 29.8% chord Max camber 6.3% at 39.8% chord Max Cl/Cd 86.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(hq308-il) HQ 3.0/8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.0/8 R/C sailplane airfoil Max thickness 8% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 86.1 at Re# 200,000 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 86.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(arad6-il) ARA-D 6% AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Aeronautical Research Association/Bocci-Dowty Rotol ARA-D 6% thick propeller airfoil Max thickness 6% at 20% chord Max camber 5% at 45% chord Max Cl/Cd 86 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe195-il) GOE 195 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 195 airfoil Max thickness 8.6% at 20% chord Max camber 5.1% at 50% chord Max Cl/Cd 86 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe342-il) GOE 342 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 342 airfoil Max thickness 5.4% at 20% chord Max camber 6.2% at 40% chord Max Cl/Cd 85.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx76mp120-il) FX 76-MP-120		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 76-MP-120 airfoil Max thickness 12.1% at 33.9% chord Max camber 7.6% at 46.7% chord Max Cl/Cd 85.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e853-il) EPPLER E853 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E853 propeller airfoil Max thickness 11.6% at 37.1% chord Max camber 3.1% at 56.1% chord Max Cl/Cd 85.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database