2D Blade Airfoil Outer Booundry
I just have a quick question;
how can we create 2D blade airfoil outer boundary as shown in attached pic?
Basically it is a periodic boundary is there any mathematical relation or equations if yes pls let me know where i can get it?
Thank you and Regards,
Create top boundary and translate it down to get bottom boundary. Do similarly for the left/right boundaries.
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