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.

(goe403-il) GOE 403 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 403 airfoil Max thickness 6.7% at 29.9% chord Max camber 4.3% at 39.9% chord Max Cl/Cd 92.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe198-il) GOE 198 (L.F.G. 5294) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 198 (L.F.G. 5294) airfoil Max thickness 7.8% at 19.9% chord Max camber 6.5% at 39.9% chord Max Cl/Cd 92.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe13k-il) GOE 13K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 13K airfoil Max thickness 14.8% at 50% chord Max camber 5.5% at 60% chord Max Cl/Cd 92.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe228-il) GOE 228 (MVA H.38) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 228 (MVA H.38) airfoil Max thickness 17.9% at 29.4% chord Max camber 7% at 49.4% chord Max Cl/Cd 92.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(s2055-il) S2055		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S2055 low Reynolds number airfoil Max thickness 8% at 34.8% chord Max camber 1.4% at 44.6% chord Max Cl/Cd 92.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(goe15k-il) GOE 15K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 15K airfoil Max thickness 15% at 50% chord Max camber 3.4% at 50% chord Max Cl/Cd 92.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(vr7b-il) BOEING-VERTOL VR-7 AIRFOIL WITH TAB		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing-Vertol VR-7 rotorcraft airfoil with tab Max thickness 12% at 33% chord Max camber 3% at 29% chord Max Cl/Cd 92.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(clarkx-il) CLARK X AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	CLARK X airfoil Max thickness 11.7% at 30% chord Max camber 3.3% at 40% chord Max Cl/Cd 92.8 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 92.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(geminism-il) GEMINI (smoothed)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	GEMINI R/C sailplane airfoil (smoothed) Max thickness 15.4% at 34.2% chord Max camber 2.2% at 37.9% chord Max Cl/Cd 92.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database