Aeroelastic Experiments - Very High Aspect Ratio Wing

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  • เผยแพร่เมื่อ 22 ต.ค. 2024

ความคิดเห็น • 8

  • @meghnasingh4396
    @meghnasingh4396 3 ปีที่แล้ว +1

    wonderful!

  • @ДанилаМартьянов-ю2н
    @ДанилаМартьянов-ю2н 4 หลายเดือนก่อน

    Hi! Do you know anyone who ever broke a wing in a tube specifically due to its divergence and got it on video? Cause I guess on the video I see an appearance of flutter at speeds that are almost equal to critical flutter speed
    I mean, its basically wing overbend, but still..

    • @danilevin868
      @danilevin868  4 หลายเดือนก่อน

      Hey
      Look for a video called Flutter at a glance, bunch of videos from NASA wind tunnels, there you can see things break.
      In the current video you see the wing fluttering beyond the linear flutter limit, hence the LCO.

    • @ДанилаМартьянов-ю2н
      @ДанилаМартьянов-ю2н 4 หลายเดือนก่อน

      @@danilevin868 I appreciate

  • @vijayreddy5728
    @vijayreddy5728 2 ปีที่แล้ว +1

    What effect can adding a mass(for example, engine) at the anti-node of that mode of vibration have? Please explain.

    • @danilevin868
      @danilevin868  2 ปีที่แล้ว +1

      By anti node do you mean the max deflection point? Adding mass w/o stiffness will lower the flutter speed, potentially adding more complex modes of vibration. It's easy to check with basic FE code and ZAERO

    • @vijayreddy5728
      @vijayreddy5728 2 ปีที่แล้ว +1

      @@danilevin868 Thank @ Dani Levin. I was under the hope, if adding mass can damp energy received by the structure from air and increased flutter speed. Can you please share some literature in support, so that I ll understand the physics of it correctly. Please bare with me, I am a beginner in aeroelasticity.

    • @danilevin868
      @danilevin868  2 ปีที่แล้ว

      @@vijayreddy5728 you can start by watching the Aeroelasticity lecture series on my channel.