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Airfoil database list (G).

GOE 373 AIRFOIL to GOE 393 AIRFOIL

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(goe373-il) GOE 373 AIRFOIL

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GOE 373 AIRFOILGottingen 373 airfoil
Max thickness 6.5% at 29.9% chord
Max camber 5.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe374-il) GOE 374 AIRFOIL

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GOE 374 AIRFOILGottingen 374 airfoil
Max thickness 6.5% at 30% chord
Max camber 4.5% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe375-il) GOE 375 AIRFOIL

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GOE 375 AIRFOILGottingen 375 airfoil
Max thickness 6.5% at 20% chord
Max camber 4.5% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe376-il) GOE 376 AIRFOIL

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GOE 376 AIRFOILGottingen 376 airfoil
Max thickness 6.6% at 30% chord
Max camber 5% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe377-il) GOE 377 AIRFOIL

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GOE 377 AIRFOILGottingen 377 airfoil
Max thickness 6.5% at 30% chord
Max camber 3.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe379-il) GOE 379 AIRFOIL

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GOE 379 AIRFOILGottingen 379 airfoil
Max thickness 6.5% at 30% chord
Max camber 5.2% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe380-il) GOE 380 AIRFOIL

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GOE 380 AIRFOILGottingen 380 airfoil
Max thickness 6.6% at 30% chord
Max camber 5.6% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe381-il) GOE 381 AIRFOIL

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GOE 381 AIRFOILGottingen 381 airfoil
Max thickness 6.4% at 30% chord
Max camber 5.8% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe382-il) GOE 382 AIRFOIL

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GOE 382 AIRFOILGottingen 382 airfoil
Max thickness 20% at 29% chord
Max camber 6% at 39% chord
Source UIUC Airfoil Coordinates Database

(goe383-il) GOE 383 AIRFOIL

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GOE 383 AIRFOILGottingen 383 airfoil
Max thickness 20.2% at 28.7% chord
Max camber 5% at 38.7% chord
Source UIUC Airfoil Coordinates Database

(goe384-il) GOE 384 AIRFOIL

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GOE 384 AIRFOILGottingen 384 airfoil
Max thickness 19.6% at 29.3% chord
Max camber 6.9% at 39.3% chord
Source UIUC Airfoil Coordinates Database

(goe385-il) GOE 385 AIRFOIL

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GOE 385 AIRFOILGottingen 385 airfoil
Max thickness 9.9% at 29.9% chord
Max camber 4.1% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe386-il) GOE 386 AIRFOIL

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GOE 386 AIRFOILGottingen 386 airfoil
Max thickness 20.3% at 29% chord
Max camber 5.4% at 39% chord
Source UIUC Airfoil Coordinates Database

(goe387-il) GOE 387 AIRFOIL

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GOE 387 AIRFOILGottingen 387 airfoil
Max thickness 14.9% at 30% chord
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe388-il) GOE 388 AIRFOIL

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GOE 388 AIRFOILGottingen 388 airfoil
Max thickness 10.2% at 29.9% chord
Max camber 5.4% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe389-il) GOE 389 AIRFOIL

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GOE 389 AIRFOILGottingen 389 airfoil
Max thickness 10.3% at 29.8% chord
Max camber 4% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe390-il) GOE 390 AIRFOIL

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GOE 390 AIRFOILGottingen 390 airfoil
Max thickness 20.3% at 29.2% chord
Max camber 6.9% at 39.2% chord
Source UIUC Airfoil Coordinates Database

(goe391-il) GOE 391 AIRFOIL

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GOE 391 AIRFOILGottingen 391 airfoil
Max thickness 5.1% at 40% chord
Max camber 3.2% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe392-il) GOE 392 AIRFOIL

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GOE 392 AIRFOILGottingen 392 airfoil
Max thickness 10.2% at 30% chord
Max camber 4.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe393-il) GOE 393 AIRFOIL

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GOE 393 AIRFOILGottingen 393 airfoil
Max thickness 6.1% at 19.9% chord
Max camber 4.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database
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