It would really be interesting to see windtunnel data of the morphing sections and comparing that with a panel method. I am curious as to the effect of the discontinuity of the tongue actuation on the lower aero surface. If this is a laminar flow section the effect will be significant.
It would really be interesting to see windtunnel data of the morphing sections and comparing that with a panel method. I am curious as to the effect of the discontinuity of the tongue actuation on the lower aero surface. If this is a laminar flow section the effect will be significant.
Дорого ненадёжно тупо
very interesting! what filament did you use?
a im uzbekistan