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Airfoil database list (G).

GOE 492 AIRFOIL to GOE 511 AIRFOIL

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(goe492-il) GOE 492 AIRFOIL

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GOE 492 AIRFOILGottingen 492 airfoil
Max thickness 6.2% at 29.9% chord
Max camber 3.4% at 49.9% chord
Source UIUC Airfoil Coordinates Database

(goe493-il) GOE 493 AIRFOIL

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GOE 493 AIRFOILGottingen 493 airfoil
Max thickness 14.9% at 29.3% chord
Max camber 3.4% at 49.3% chord
Source UIUC Airfoil Coordinates Database

(goe494-il) GOE 494 AIRFOIL

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GOE 494 AIRFOILGottingen 494 airfoil
Max thickness 5% at 20% chord
Max camber 5.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe495-il) GOE 495 AIRFOIL

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GOE 495 AIRFOILGottingen 495 airfoil
Max thickness 6.9% at 30% chord
Max camber 5% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe496-il) GOE 496 AIRFOIL

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GOE 496 AIRFOILGottingen 496 airfoil
Max thickness 10% at 30% chord
Max camber 5% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe497-il) GOE 497 AIRFOIL

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GOE 497 AIRFOILGottingen 497 airfoil
Max thickness 12.7% at 30% chord
Max camber 5.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe498-il) GOE 498 AIRFOIL

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GOE 498 AIRFOILGottingen 498 airfoil
Max thickness 15.9% at 29.4% chord
Max camber 5.5% at 49.4% chord
Source UIUC Airfoil Coordinates Database

(goe499-il) GOE 499 AIRFOIL

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GOE 499 AIRFOILGottingen 499 airfoil
Max thickness 6.8% at 30% chord
Max camber 5.9% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe500-il) GOE 500 AIRFOIL

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GOE 500 AIRFOILGottingen 500 airfoil
Max thickness 10% at 30% chord
Max camber 6% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe501-il) GOE 501 AIRFOIL

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GOE 501 AIRFOILGottingen 501 airfoil
Max thickness 12.8% at 30% chord
Max camber 6.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe502-il) GOE 502 AIRFOIL

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GOE 502 AIRFOILGottingen 502 airfoil
Max thickness 15.9% at 29.3% chord
Max camber 6.1% at 49.4% chord
Source UIUC Airfoil Coordinates Database

(goe503-il) GOE 503 AIRFOIL

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GOE 503 AIRFOILGottingen 503 airfoil
Max thickness 15.6% at 29.7% chord
Max camber 7% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe504-il) GOE 504 AIRFOIL

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GOE 504 AIRFOILGottingen 504 airfoil
Max thickness 18% at 29.2% chord
Max camber 5.4% at 39.2% chord
Source UIUC Airfoil Coordinates Database

(goe505-il) GOE 505 AIRFOIL

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GOE 505 AIRFOILGottingen 505 airfoil
Max thickness 14% at 19.7% chord
Max camber 5.9% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe506-il) GOE 506 AIRFOIL

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GOE 506 AIRFOILGottingen 506 airfoil
Max thickness 16.5% at 29.3% chord
Max camber 4.7% at 39.3% chord
Source UIUC Airfoil Coordinates Database

(goe507-il) GOE 507 AIRFOIL

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GOE 507 AIRFOILGottingen 507 airfoil
Max thickness 8.7% at 30% chord
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe508-il) GOE 508 AIRFOIL

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GOE 508 AIRFOILGottingen 508 airfoil
Max thickness 16.5% at 30% chord
Max camber 5.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe509-il) GOE 509 AIRFOIL

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GOE 509 AIRFOILGottingen 509 airfoil
Max thickness 11.1% at 29.9% chord
Max camber 5.2% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe510-il) GOE 510 AIRFOIL

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GOE 510 AIRFOILGottingen 510 airfoil
Max thickness 13.7% at 19.7% chord
Max camber 5.8% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe511-il) GOE 511 AIRFOIL

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GOE 511 AIRFOILGottingen 511 airfoil
Max thickness 16.6% at 19.9% chord
Max camber 8% at 29.8% chord
Source UIUC Airfoil Coordinates Database
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