ANSYS Structural Buckling Analysis

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  • Опубліковано 28 лис 2024

КОМЕНТАРІ • 47

  • @rayhansaiafbin8898
    @rayhansaiafbin8898 Рік тому +8

    The way you have presented multiple buckling types in one single video is awesome. Hats off.

  • @yatzilfajardo8612
    @yatzilfajardo8612 6 місяців тому

    Wonderful Endeavos! Thats what i needed to finish my analysis of a wing spar👏🏾👌🏾

  • @rezasadeghi2520
    @rezasadeghi2520 7 місяців тому +2

    thank you so much for sharing your knowledge, it was a great video, I really enjoyed it.

  • @naderzamani5752
    @naderzamani5752 11 місяців тому

    Thank you Endeavos Innovations. A great presentation.

  • @piotrwieckowski9401
    @piotrwieckowski9401 4 місяці тому

    Amazing video! Thank you very much! You have helped me to solve a design problem in my work ❤

    • @endeavos
      @endeavos  3 місяці тому

      Glad it helped!. You are welcome

  • @imdadimmu8741
    @imdadimmu8741 Місяць тому

    Very helpful video

  • @Arseniy_Arseniy
    @Arseniy_Arseniy 9 місяців тому

    Thank you very much for this clear explanation!
    Could you be so kind as to share the link with models' geometry?

  • @TheMonkyfunny
    @TheMonkyfunny 8 місяців тому

    Awesome sauce

  • @ihbriones
    @ihbriones Рік тому

    Great video! Thanks!

    • @endeavos
      @endeavos  Рік тому

      Glad you liked it!

    • @Arseniy_Arseniy
      @Arseniy_Arseniy 9 місяців тому

      ​​@@endeavosThank you very much for this clear explanation!
      Could you be so kind as to share the link with models' geometry or the final ansys file ?

  • @gokulrajendran7111
    @gokulrajendran7111 10 місяців тому

    nice explanation

    • @endeavos
      @endeavos  3 місяці тому

      Thanks and welcome

  • @邱勝煜-x7h
    @邱勝煜-x7h Рік тому +1

    Dear sir, thanks for a brilliant video. I'm wondering if it can couple two buckling mode shapes?

    • @endeavos
      @endeavos  Рік тому

      In some cases two buckling loads can happen successively as the buckling load is increased. Is that what you mean?

  • @AlessandroGiuliani-g9g
    @AlessandroGiuliani-g9g 3 місяці тому

    Hi, please can you explain to me the reason of 10 millimeters of displacement in the first example ( rod ) ? Thanks in advance

  • @malikfaizan4638
    @malikfaizan4638 Рік тому

    How do i scale it i didn't understood and i am getting the normal deformation not at center but at top how shall i change it

  • @hamza_ME_
    @hamza_ME_ 10 місяців тому

    Are there any specific guidelines on defining the number of steps/substeps (initial, minimum, and maximum), plus Step End Time?

    • @endeavos
      @endeavos  3 місяці тому

      My apologies for the late response. It really depends on the nonlinearity of the model.

  • @vjx385
    @vjx385 5 місяців тому

    The results I calculated are very different from those in your video. I hope to find the issue from your model.

    • @lumo9435
      @lumo9435 19 днів тому

      Hey, I happened to have a very different results as well. Would you mind sharing what you have done?

  • @IoldxmanI
    @IoldxmanI 6 місяців тому +1

    Go on, please!

  • @thymeteller6837
    @thymeteller6837 Рік тому

    Dear sir, thank you so much for a very comprehensive video, I was wondering which statement in DNV-RP-C208 implied that the capacity is "200 ish" kN, as you mentioned at 37:50 mins. of the video.

    • @endeavos
      @endeavos  Рік тому

      Thanks for watching. The ~200+ KN is the estimated capacity based on DNV's chart. it is marked right there on Fig B-17.

    • @mikeb1097
      @mikeb1097 9 місяців тому

      @@endeavosThe ~210 kN is not the 'allowable limit' based on the non-linear buckling. The 210 kN is the unfactored capacity from the previous example which was based on LBA and empirical buckling curves. The design capacity from NLA is the max value on the chart divided by all relevant safety factors (load and resistance) based on whatever code you are working to.

  • @drury2d8
    @drury2d8 Рік тому

    16:16 I think the scale factor is not 15 mm, rather is 15 times the deformation of the linearized eigenmode shape. Please correct me if im wrong here.

    • @endeavos
      @endeavos  Рік тому

      The linear buckling load is normalized to unit deformation. So I can use scale factor = deformation.

  • @fatimahseba6930
    @fatimahseba6930 4 місяці тому

    How did you create the chart? 18:39

  • @balar1804
    @balar1804 Рік тому

    For Non linear thermal buckling , how to find the critical buckling temperature

    • @endeavos
      @endeavos  Рік тому

      Temperature can impact young's modulus if you have defined it as function of temperature. Buckling can happen at any temperature. There is no set "buckling temperature". If you want to find how buckling load varies with increasing temperature, you may have to run this simulation at different temperatures by inserting temperature as a load. You can use the temperature as a parameter and run this simulation at different temperatures to determine buckling load as a function of temperature.

    • @balar1804
      @balar1804 Рік тому

      @@endeavos i assumed temperature is constant, only temperature varies across the thickness.

  • @nuraisyahsamsul2831
    @nuraisyahsamsul2831 Рік тому

    why i cannot change the material properties from linear to non linear?

    • @endeavos
      @endeavos  Рік тому

      I didn't get your question. Can you elaborate it?

    • @nuraisyahsamsul2831
      @nuraisyahsamsul2831 Рік тому

      @@endeavos sorry, i get it now, i want to change my question, what is the different between force based and displacement based analysis, and why both of analysis we get the similar result?
      Another question, why i cannot get the graph like you did? I m getting straight line. 😣

    • @endeavos
      @endeavos  Рік тому

      @@nuraisyahsamsul2831 In the force based analysis, we apply a force to initiate buckling which results in displacement whereas in the displacement based analysis, we apply displacement to initiate buckling. Both methods will give you the same buckling load, however, force based methods run into convergence problems. Displacement based loading is preferred because it will also show you post buckled behavior of the structure.

    • @endeavos
      @endeavos  Рік тому

      @@nuraisyahsamsul2831 Regarding the second question, can you tell me what example or problem you are referring to?

  • @gunner4238
    @gunner4238 Рік тому

    Hi, I am confused how you came up with the scale factor at 16:16, and does this work on all geometry like corrugated walls?

    • @endeavos
      @endeavos  Рік тому

      Hi Benjamin. The scale factor is based on the manufacturing tolerance and as structural designer, it is basically your choice. If you want to be conservative, you can use the max tolerance. In this video, I followed the DNV's recommendation. Please see the document DNV-RP-C208. Thanks!

    • @gunner4238
      @gunner4238 Рік тому

      @@endeavos Thanks for the information! Can I also know which section did you get the value from? And another question I would like to ask is: In my project, I need to apply both hydrostatic and constant pressure onto a corrugated wall. When I get my eigenvalue, do I multiply the eigenvalue to both pressure or just the constant pressure? Thanks in advance!

  • @imdadimmu8741
    @imdadimmu8741 Місяць тому

    I m research scholar and I need your help in my research work

  • @nuraisyahsamsul2831
    @nuraisyahsamsul2831 Рік тому

    Hi, can i have your email, i want to ask about my problem regarding my project

    • @endeavos
      @endeavos  Рік тому

      Sure, its zaeem@endeavos.com