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.

(as5048-il) AS5048 (18%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	AS5048 airfoil Ashok Gopalarathnam/Selig 18% airfoil Max thickness 18% at 38.3% chord Max camber 0.8% at 77.8% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(sc20012-il) NASA SC(2)-0012 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NASA SC(2)-0012 airfoil (NASA TP-2969) Max thickness 12% at 37% chord Max camber 0% at 0% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe329-il) GOE 329 (PFALZ 58) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 329 (Pfalz 58) airfoil Max thickness 10.2% at 29.9% chord Max camber 5.5% at 29.9% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(nacam2-il) NACA M2		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA M2 airfoil Max thickness 8.1% at 30% chord Max camber 0% at 0% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(sc1012r8-il) SIKORSKY SC1012R8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Sikorsky SC1012 R8 rotorcraft airfoil Max thickness 12% at 27.8% chord Max camber 2.7% at 21.8% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(s3-il) REPUBLIC S-3 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Republic S-3 airfoil (P-47 wing airfoil) Max thickness 11% at 30% chord Max camber 1.8% at 15% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(m23-il) NACA M23 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-23 airfoil Max thickness 8.1% at 30.1% chord Max camber 6.4% at 30.1% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(b737b-il) BOEING 737 MIDSPAN AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing Commercial Airplane Company model 737 airfoils Max thickness 12.5% at 29.7% chord Max camber 0.8% at 10% chord Max Cl/Cd 23.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(v43015-il) BOEING VERTOL V43015-2.48 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing-Vertol V43015-2.48 rotorcraft airfoil Max thickness 15% at 30% chord Max camber 3.7% at 15% chord Max Cl/Cd 23.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe436-il) GOE 436 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 436 airfoil Max thickness 11% at 30% chord Max camber 3.8% at 30% chord Max Cl/Cd 23.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database