Youtor
NACA0012 airfoil with deploying spoiler
>> YOUR LINK HERE: ___ http://youtube.com/watch?v=H-snLmMQK0Y
Software used: https://github.com/vvflow/vvflow • Process of spoiler deviation is being modeling using method of viscous vortex domains (VVD). Re = 40 000. Spoiler size is 10% of chord, spoiler's trailing edge is 20% far from airfoil's trailing edge. Angle of attack = 0. • Equations: Navier-Stokes; • BC: no-slip at the surface, no-perturbations at infinity
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