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Airfoil database list (G).

GOE 777 AIRFOIL to UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL

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(goe777-il) GOE 777 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 777 airfoil Max thickness 22% at 30% chord Max camber 5.9% at 30% chord Source UIUC Airfoil Coordinates Database
(goe780-il) GOE 780 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 780 airfoil Max thickness 12% at 50% chord Max camber 1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe79-il) GOE 79 (PFALZ 11) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 79 (Pfalz 11) airfoil Max thickness 6.2% at 14.9% chord Max camber 6% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe795-il) GOE 795 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 795 airfoil Max thickness 8% at 30.9% chord Max camber 2.4% at 43.5% chord Source UIUC Airfoil Coordinates Database
(goe795sm-il) GOE 795 smoothed		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 795 airfoil (smoothed) Max thickness 8% at 30.9% chord Max camber 2.4% at 43.5% chord Source UIUC Airfoil Coordinates Database

(goe796-il) GOE 796 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 796 airfoil Max thickness 12% at 30% chord Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database
(goe797-il) GOE 797 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 797 airfoil Max thickness 16% at 30% chord Max camber 4.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe798-il) GOE 798 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 798 airfoil Max thickness 20% at 30% chord Max camber 6% at 40% chord Source UIUC Airfoil Coordinates Database
(goe801-il) GOE 801 (MVA 301) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 801 (MVA 301) airfoil Max thickness 9.8% at 30% chord Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe802-il) GOE 802 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 802 airfoil Max thickness 9.8% at 30% chord Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe802a-il) GOE 802 A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 802 A airfoil Max thickness 9.8% at 30% chord Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe802b-il) GOE 802 B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 802 B airfoil Max thickness 9.8% at 30% chord Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe803h-il) GOE 803 (HACKLINGER) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 803 (Hacklinger) airfoil Max thickness 6.3% at 15% chord Max camber 6.6% at 40% chord Source UIUC Airfoil Coordinates Database

(goe804-il) GOE 804 (EA 8) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 804 (EA 8) airfoil Max thickness 6% at 40% chord Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database
(goe81-il) GOE 81 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 81 airfoil Max thickness 7.4% at 29.9% chord Max camber 6.3% at 29.9% 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
(griffith30symsuction-il) Griffith 30% Suction Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(gs1-il) SIKORSKY GS-1 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gluharoff/Sikorsky GS-1 airfoil Max thickness 13.9% at 30% chord Max camber 4.1% at 50% chord Source UIUC Airfoil Coordinates Database
(gu255118-il) UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Glasgow GU 25-5(11)8 canard airfoil (Quickie Max thickness 20% at 40% chord Max camber 7.1% at 45% chord Source UIUC Airfoil Coordinates Database