8. ONR YIP Final Presentation - Morphing Wing Design - Moulton

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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.

zaflytech
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very interesting! what filament did you use?

enriquetabora
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