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Airfoil database list (G).

GOE 574 AIRFOIL to GOE 610-B MOD. AIRFOIL

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(goe574-il) GOE 574 AIRFOIL

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GOE 574 AIRFOILGottingen 574 airfoil
Max thickness 10.3% at 30% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe575-il) GOE 575 AIRFOIL

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GOE 575 AIRFOILGottingen 575 airfoil
Max thickness 13.3% at 29.8% chord
Max camber 3.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe584-il) GOE 584 AIRFOIL

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GOE 584 AIRFOILGottingen 584 airfoil
Max thickness 12.7% at 30% chord
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe585-il) GOE 585 AIRFOIL

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GOE 585 AIRFOILGottingen 585 airfoil
Max thickness 8.2% at 20% chord
Max camber 3.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe587-il) GOE 587 AIRFOIL

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GOE 587 AIRFOILGottingen 587 airfoil
Max thickness 5.8% at 40% chord
Max camber 3% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe590-il) GOE 590 AIRFOIL

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GOE 590 AIRFOILGottingen 590 airfoil
Max thickness 5.7% at 30% chord
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe591-il) GOE 591 AIRFOIL

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GOE 591 AIRFOILGottingen 591 airfoil
Max thickness 11.2% at 30% chord
Max camber 5.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe592-il) GOE 592 AIRFOIL

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GOE 592 AIRFOILGottingen 592 airfoil
Max thickness 14.3% at 29.7% chord
Max camber 7.5% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe593-il) GOE 593 AIRFOIL

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GOE 593 AIRFOILGottingen 593 airfoil
Max thickness 11.9% at 30% chord
Max camber 4.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe595-il) GOE 595 AIRFOIL

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GOE 595 AIRFOILGottingen 595 airfoil
Max thickness 9.6% at 30% chord
Max camber 3% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe596-il) GOE 596 AIRFOIL

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GOE 596 AIRFOILGottingen 596 airfoil
Max thickness 9.8% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe598-il) GOE 598 AIRFOIL

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GOE 598 AIRFOILGottingen 598 airfoil
Max thickness 6.5% at 39.8% chord
Max camber 1% at 49.8% chord
Source UIUC Airfoil Coordinates Database

(goe599-il) GOE 599 AIRFOIL

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GOE 599 AIRFOILGottingen 599 airfoil
Max thickness 10% at 29.6% chord
Max camber 1.5% at 59.7% chord
Source UIUC Airfoil Coordinates Database

(goe600-il) GOE 600 AIRFOIL

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GOE 600 AIRFOILGottingen 600 airfoil
Max thickness 13.1% at 29.4% chord
Max camber 1.9% at 49.4% chord
Source UIUC Airfoil Coordinates Database

(goe601-il) GOE 601 AIRFOIL

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GOE 601 AIRFOILGottingen 601 airfoil
Max thickness 16% at 39% chord
Max camber 2.5% at 49% chord
Source UIUC Airfoil Coordinates Database

(goe602-il) GOE 602 AIRFOIL

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GOE 602 AIRFOILGottingen 602 airfoil
Max thickness 10% at 30% chord
Max camber 3.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe602m-il) GOE 602 MOD. AIRFOIL

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GOE 602 MOD. AIRFOILGottingen 602 MOD airfoil
Max thickness 9.6% at 30% chord
Max camber 3.8% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe604-il) GOE 604 AIRFOIL

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GOE 604 AIRFOILGottingen 604 airfoil
Max thickness 17.8% at 29.3% chord
Max camber 5.4% at 29.3% chord
Source UIUC Airfoil Coordinates Database

(goe610b-il) GOE 610 B AIRFOIL

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GOE 610 B AIRFOILGottingen 610 B airfoil
Max thickness 7.8% at 39.9% chord
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe610bm-il) GOE 610-B MOD. AIRFOIL

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GOE 610-B MOD. AIRFOILGottingen 610-B MOD airfoil
Max thickness 7.7% at 30% chord
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
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