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.

(goe257-il) GOE 257 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 257 airfoil Max thickness 8.8% at 30% chord Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database
(goe490-il) GOE 490 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 490 airfoil Max thickness 8.8% at 19.9% chord Max camber 3.8% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe92-il) GOE 92 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 92 airfoil Max thickness 8.8% at 30% chord Max camber 5.5% at 30% chord Source UIUC Airfoil Coordinates Database
(mh121-il) MH 121 8.76%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 121 for tip section of a propeller Max thickness 8.8% at 37.9% chord Max camber 3% at 62.2% chord Source UIUC Airfoil Coordinates Database
(ag35-il) AG35		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG35 airfoil Max thickness 8.7% at 27.9% chord Max camber 2.3% at 37% chord Source UIUC Airfoil Coordinates Database
(e178-il) E178 (8.69%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E178 low Reynolds number airfoil Max thickness 8.7% at 29.8% chord Max camber 2.8% at 38.8% chord Source UIUC Airfoil Coordinates Database
(goe180-il) GOE 180 (MVA H.26) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 180 (MVA H.26) airfoil Max thickness 8.7% at 30% chord Max camber 4.4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe274-il) GOE 274 (DAIMLER V) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 274 (DAIMLER V) airfoil Max thickness 8.7% at 29.9% chord Max camber 4.8% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe507-il) GOE 507 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 507 airfoil Max thickness 8.7% at 30% chord Max camber 2.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe566-il) GOE 566 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 566 airfoil Max thickness 8.7% at 30% chord Max camber 2.6% at 40% chord Source UIUC Airfoil Coordinates Database

Page 128 of 164     118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137     Next

Please see the source web site or designer for any license conditions.