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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

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GOE 777 AIRFOILGottingen 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

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GOE 780 AIRFOILGottingen 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

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GOE 79 (PFALZ 11) AIRFOILGottingen 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

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GOE 795 AIRFOILGottingen 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

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GOE 795 smoothedGottingen 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

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GOE 796 AIRFOILGottingen 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

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GOE 797 AIRFOILGottingen 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

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GOE 798 AIRFOILGottingen 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

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GOE 801 (MVA 301) AIRFOILGottingen 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

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GOE 802 AIRFOILGottingen 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

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GOE 802 A AIRFOILGottingen 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

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GOE 802 B AIRFOILGottingen 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

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GOE 803 (HACKLINGER) AIRFOILGottingen 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

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GOE 804 (EA 8) AIRFOILGottingen 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

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GOE 81 AIRFOILGottingen 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

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GOE 92 AIRFOILGottingen 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

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Griffith 30% Suction AirfoilGriffith 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

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SIKORSKY GS-1 AIRFOILGluharoff/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

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UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOILUniversity 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
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