NACA 66021 3d model
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NACA 66021

NACA 66021

by GrabCAD
Last crawled date: 2 years ago
Airfoil for pylon race plane

(n66021-il) NACA 66-021 AIRFOIL
NACA 66(4)-021 airfoil
Max thickness 21% at 45% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

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