Stress Analysis II: L-17 Stability - Buckling of Flat Plates

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  • Опубликовано: 27 окт 2024

Комментарии • 5

  • @kgajjar3219
    @kgajjar3219 2 года назад +1

    flexural rigidity: has information about "per unit inch" 11:00 ish
    tension relationship with buckling by stress ratio + interaction equations around 44:00
    infinitely fixed = clamped 33:00

  • @mexguit
    @mexguit Год назад +1

    Hello Mr. Coburn. I’ve been looking for a shear web with two holes but can’t find it. I have with one hole and how to calculate doubler reinforcement but can’t find with two holes. Have you seen that type of design and analysis before?

    • @ToddCoburn
      @ToddCoburn  Год назад +2

      Thanks for asking. Michael Niu’s “Airframe Structural Design” has a method in chp 6 based on a Saab report that is pretty good. He has other guidance and analysis methods that can be employed with modification as well.
      Michael Niu’s Airframe Stress Analysis & Sizing has additional material on that as well in Chp 13.
      Jean Claude Flabel’s “ Practical Stress Analysis for Design Engineers” chp 9 provides analysis guidlines that can also be employed

    • @mexguit
      @mexguit Год назад +1

      Thank you for your reply. I will check these out.