UNSW - Aerospace Structures - Buckling of Stiffened Panels

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  • เผยแพร่เมื่อ 28 พ.ค. 2014
  • Buckling of Stiffened Panels
    - Buckling Modes
    - Effective Width
    - Crippling
    - Design of Stiffened Panels
    Information is for educational use and should be viewed in this context. If you are building/analysing/designing a real aircraft, good luck to you, but seek your own professional advice.

ความคิดเห็น • 10

  • @jeremygunetilleke7672
    @jeremygunetilleke7672 9 ปีที่แล้ว +3

    Hi, these are brilliant videos! I am currently teaching myself about aircraft stresses and loads. These are great explanations and help when used alongside textbooks. Is there any way that we can access the rest of the lecture videos? Many thanks

  • @sebastianvalencia1846
    @sebastianvalencia1846 6 ปีที่แล้ว

    Great!!!

  • @netflixhd265
    @netflixhd265 6 ปีที่แล้ว

    Great!!

  • @tinu8515
    @tinu8515 3 ปีที่แล้ว

    Please make a video about Postbuckling analysis of stiffened functionally graded material plate using Abaqus software

  • @karanthtradingroom4839
    @karanthtradingroom4839 9 หลายเดือนก่อน

    Great video.. do you have any examples to show both hand calculations and FEM analysis..

  • @birthmark85
    @birthmark85 5 ปีที่แล้ว

    Thanks for uploading this, it's very usefull. Where can I find the first image of the wing section shown in the first slide?

    • @AerospaceStructures
      @AerospaceStructures  5 ปีที่แล้ว +2

      This is from a book called "Practical Stress Analysis for Design Engineers" by Flabel. It is actually out of print at the moment unfortunately, you might have to track it down through a library.

  • @prajwalgautam4015
    @prajwalgautam4015 ปีที่แล้ว

    1:21:00 number of edges in stiffener

    • @shankarmallaSBM
      @shankarmallaSBM ปีที่แล้ว

      kada comment handini yr
      last kada padhdini yr