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Airfoil database list (G).

GOE 512 AIRFOIL to GOE 54 AIRFOIL

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(goe512-il) GOE 512 AIRFOIL

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GOE 512 AIRFOILGottingen 512 airfoil
Max thickness 13.9% at 19.9% chord
Max camber 5.6% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe513-il) GOE 513 AIRFOIL

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GOE 513 AIRFOILGottingen 513 airfoil
Max thickness 16.6% at 29.8% chord
Max camber 5.2% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe514-il) GOE 514 AIRFOIL

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GOE 514 AIRFOILGottingen 514 airfoil
Max thickness 16.6% at 19.7% chord
Max camber 6.4% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe515-il) GOE 515 AIRFOIL

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GOE 515 AIRFOILGottingen 515 airfoil
Max thickness 8.5% at 30% chord
Max camber 2.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe517-il) GOE 517 AIRFOIL

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GOE 517 AIRFOILGottingen 517 airfoil
Max thickness 7% at 30% chord
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe518-il) GOE 518 AIRFOIL

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GOE 518 AIRFOILGottingen 518 airfoil
Max thickness 18% at 29.8% chord
Max camber 7.3% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe522-il) GOE 522 AIRFOIL

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GOE 522 AIRFOILGottingen 522 airfoil
Max thickness 21.8% at 28.6% chord
Max camber 5.2% at 48.7% chord
Source UIUC Airfoil Coordinates Database

(goe523-il) GOE 523 AIRFOIL

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GOE 523 AIRFOILGottingen 523 airfoil
Max thickness 16.5% at 29.7% chord
Max camber 9.7% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe525-il) GOE 525 AIRFOIL

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GOE 525 AIRFOILGottingen 525 airfoil
Max thickness 16.5% at 29.7% chord
Max camber 9.7% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe526-il) GOE 526 AIRFOIL

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GOE 526 AIRFOILGottingen 526 airfoil
Max thickness 12.3% at 29.7% chord
Max camber 4.1% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe527-il) GOE 527 AIRFOIL

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GOE 527 AIRFOILGottingen 527 airfoil
Max thickness 16.5% at 29.5% chord
Max camber 5.8% at 39.5% chord
Source UIUC Airfoil Coordinates Database

(goe528-il) GOE 528 AIRFOIL

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GOE 528 AIRFOILGottingen 528 airfoil
Max thickness 12.5% at 29.8% chord
Max camber 6.2% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe529-il) GOE 529 AIRFOIL

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GOE 529 AIRFOILGottingen 529 airfoil
Max thickness 9.7% at 29.9% chord
Max camber 5.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe530-il) GOE 530 AIRFOIL

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GOE 530 AIRFOILGottingen 530 airfoil
Max thickness 12.9% at 29.8% chord
Max camber 5.1% at 29.8% chord
Source UIUC Airfoil Coordinates Database

(goe531-il) GOE 531 AIRFOIL

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GOE 531 AIRFOILGottingen 531 airfoil
Max thickness 13.8% at 19.5% chord
Max camber 14.7% at 49.3% chord
Source UIUC Airfoil Coordinates Database

(goe532-il) GOE 532 AIRFOIL

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GOE 532 AIRFOILGottingen 532 airfoil
Max thickness 12.5% at 30% chord
Max camber 4.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe533-il) GOE 533 AIRFOIL

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GOE 533 AIRFOILGottingen 533 airfoil
Max thickness 13.7% at 30% chord
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe534-il) GOE 534 AIRFOIL

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GOE 534 AIRFOILGottingen 534 airfoil
Max thickness 14.1% at 19.6% chord
Max camber 5.2% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(goe535-il) GOE 535 AIRFOIL

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GOE 535 AIRFOILGottingen 535 airfoil
Max thickness 16.1% at 20% chord
Max camber 5.8% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe54-il) GOE 54 AIRFOIL

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GOE 54 AIRFOILGottingen 54 airfoil
Max thickness 6.5% at 14.9% chord
Max camber 3.5% at 19.9% chord
Source UIUC Airfoil Coordinates Database
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