0526

OTHER: Aerodynamics - Blade Profile - NACA 0009

For information related to the specific blade for the Unicopter see: UniCopter ~ Rotor - Blade - NACA 00xx

Drawing:

 

 Characteristics:

Thickness

t/c

= 0.09

Leading Edge Circle

r/c

= 0.89

Center at

x/c

=

Center at

y/c

=

The maximum coefficient of lift (clMax) is approximately 1.3 at 14.5º angle of attack. [Source ~ TWS p.462]

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Last Revised: Sunday, February 11, 2009