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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.

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(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

(hh02-il) HUGHES HELICOPTERS HH-02 AIRFOIL

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HUGHES HELICOPTERS HH-02 AIRFOILHughes helicopters HH-02 rotorcraft airfoil
Max thickness 9.6% at 30% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(hobie-il) HOBIE

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HOBIEHobie Hawk airfoil (Hobie Hawk R/C sailplane)
Max thickness 8.5% at 25% chord
Max camber 4% at 45% chord
Source UIUC Airfoil Coordinates Database
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