How to calculate critical bending moment

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  • Опубликовано: 11 сен 2024
  • Free FEA course: enterfea.com/i...
    This video was made for a post on my blog. You can find it here: enterfea.com/ho...
    Thank you for watching and have a great day!

Комментарии • 13

  • @ukaszRadzikRB
    @ukaszRadzikRB 7 лет назад +1

    Perfect and very useful material!

    • @Enterfea
      @Enterfea  7 лет назад

      Thanks, I'm glad you like it :)

  • @BillySnowball
    @BillySnowball 2 года назад +1

    Good job, I need to get me a copy of RFEM

    • @Enterfea
      @Enterfea  2 года назад +1

      Thanks! I would recommend RFEM for sure :) I like the RFEM5 version better than RFEM6, but maybe it's a matter of habit :)

    • @BillySnowball
      @BillySnowball 2 года назад +1

      @@Enterfea So I used different software to solve my problem as the extrusion was quite a complicated shape. Whilst bench marking using your example there was about a 20% difference between 8 node brick elements and 20 node brick elements. Matching the support conditions as closely as possible the 20 node brick matched CBF ~ 0.74 whilst the 8 node CBF was ~ 0.55. Any ideas on why there would be such a big difference just on the element type used?

    • @Enterfea
      @Enterfea  2 года назад +1

      @@BillySnowball this is a complicated thing Mate, but assuming that you had the same element "size", but the difference was HEX20 or HEX8, I can imagine such a difference. This is what mesh convergence is for - it would allow you to see, how small elements are needed (and you do it separately for HES8 and HEX20). You can read more here (enterfea.com/mesh-convergence/), although I'm using QUAD (2D) elements in the example (but still first and second order, so it should give you an idea about what is going on :) ). Hope this helps!

    • @BillySnowball
      @BillySnowball 2 года назад +1

      @@Enterfea I appreciate you spending the time to respond. I think I've read your website before and will definitely check out the page you linked. Thanks again

    • @Enterfea
      @Enterfea  2 года назад

      @@BillySnowball Sure thing! Best of luck!

  • @NTC
    @NTC 6 лет назад +1

    it's a great method !

    • @Enterfea
      @Enterfea  6 лет назад

      Hey! I'm really glad that you like it :)
      All the best
      Ł

    • @bengthebrazilianengineerinAus
      @bengthebrazilianengineerinAus 3 года назад

      Tien C. Nguyen...can you achieve something similar in Spacegass?

    • @NTC
      @NTC 3 года назад +1

      @@bengthebrazilianengineerinAus You definitely can. Just use shell elements to model the span, then run the buckling analysis. FYI: In the future release of SG, you can predict the lateral-torsional buckling load factor using beam elements directly.

    • @bengthebrazilianengineerinAus
      @bengthebrazilianengineerinAus 3 года назад

      @@NTC Awesome. Will give it a try. That's great news. Looking forward to it . Cheers