Airfoil Tools
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Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil database search

Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

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(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

(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
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