Abhilash Pullayikkodi

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Kanhangad, India

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HOW can i get the coordinate data from an airfoil graphics?

Abhilash Pullayikkodi
in Design & CAD
2 0 Intermediate
You can obtain all the geometric data from the name itself. The airofoil name 63-621 was given. .The NACA 63621 profile describes an airfoil with design lift coefficient of 0.9 (0.15*6), the point of maximum camber located at 15% chord (5*3), reflex camber, and maximum thickness of 21% of chord length (21). Other details are irrelevant visit http://airfoiltools.com/airfoil/naca5digit for more information.
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How to make this?(given in the link)....https://d2t1xqejof9utc.cloudfront.net/pictures/files/10546/large.jpg?1332899233

Abhilash Pullayikkodi
in Design & CAD
1 0 Intermediate
The design is simple...
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