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Airfoil database list (G).

GOE 546 AIRFOIL to GOE 573 AIRFOIL

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(goe546-il) GOE 546 AIRFOIL

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GOE 546 AIRFOILGottingen 546 airfoil
Max thickness 10.4% at 30% chord
Max camber 3.6% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe547-il) GOE 547 AIRFOIL

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GOE 547 AIRFOILGottingen 547 airfoil
Max thickness 10.5% at 29.7% chord
Max camber 4% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe548-il) GOE 548 AIRFOIL

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GOE 548 AIRFOILGottingen 548 airfoil
Max thickness 11.9% at 40% chord
Max camber 2.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe549-il) GOE 549 AIRFOIL

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GOE 549 AIRFOILGottingen 549 airfoil
Max thickness 13.9% at 30% chord
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe55-il) GOE 55 AIRFOIL

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GOE 55 AIRFOILGottingen 55 airfoil
Max thickness 6.2% at 14.9% chord
Max camber 2% at 19.9% chord
Source UIUC Airfoil Coordinates Database

(goe550-il) GOE 550 AIRFOIL

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GOE 550 AIRFOILGottingen 550 airfoil
Max thickness 13% at 20% chord
Max camber 4.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe553-il) GOE 553 AIRFOIL

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GOE 553 AIRFOILGottingen 553 airfoil
Max thickness 13.7% at 29.6% chord
Max camber 4.7% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(goe559-il) GOE 559 AIRFOIL

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GOE 559 AIRFOILGottingen 559 airfoil
Max thickness 11.2% at 30% chord
Max camber 3.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe561-il) GOE 561 AIRFOIL

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GOE 561 AIRFOILGottingen 561 airfoil
Max thickness 25% at 29.8% chord
Max camber 10.2% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe562-il) GOE 562 AIRFOIL

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GOE 562 AIRFOILGottingen 562 airfoil
Max thickness 14.1% at 30% chord
Max camber 6.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe563-il) GOE 563 AIRFOIL

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GOE 563 AIRFOILGottingen 563 airfoil
Max thickness 8.9% at 29.8% chord
Max camber 2.2% at 49.8% chord
Source UIUC Airfoil Coordinates Database

(goe564-il) GOE 564 AIRFOIL

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GOE 564 AIRFOILGottingen 564 airfoil
Max thickness 8.2% at 30% chord
Max camber 2.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe565-il) GOE 565 AIRFOIL

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GOE 565 AIRFOILGottingen 565 airfoil
Max thickness 8.4% at 30% chord
Max camber 2.8% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe566-il) GOE 566 AIRFOIL

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GOE 566 AIRFOILGottingen 566 airfoil
Max thickness 8.7% at 30% chord
Max camber 2.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe567-il) GOE 567 AIRFOIL

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GOE 567 AIRFOILGottingen 567 airfoil
Max thickness 14.8% at 29.5% chord
Max camber 5.3% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe57-il) GOE 57 AIRFOIL

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GOE 57 AIRFOILGottingen 57 airfoil
Max thickness 6.3% at 19.9% chord
Max camber 5.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe570-il) GOE 570 AIRFOIL

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GOE 570 AIRFOILGottingen 570 airfoil
Max thickness 33.7% at 30% chord
Max camber 9.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe571-il) GOE 571 AIRFOIL

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GOE 571 AIRFOILGottingen 571 airfoil
Max thickness 24.9% at 29.4% chord
Max camber 9.8% at 29.4% chord
Source UIUC Airfoil Coordinates Database

(goe572-il) GOE 572 AIRFOIL

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GOE 572 AIRFOILGottingen 572 airfoil
Max thickness 18.6% at 29.9% chord
Max camber 8.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe573-il) GOE 573 AIRFOIL

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GOE 573 AIRFOILGottingen 573 airfoil
Max thickness 14.1% at 29.9% chord
Max camber 6.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database
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