Modal Analysis Using The Normal Mode Method

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  • Опубликовано: 6 июл 2024
  • Decoupling of the equations of motion by transforming them into the system's normal coordinates. We derive the theory behind the transformation step-by-step and work an example to demonstrate the method.
    Download notes for THIS video HERE: bit.ly/3YbFL4j
    Download notes for my other videos: bit.ly/37OH9lX
    LINKS:
    Two Degree of Freedom Problem Without Damping
    • Two Degree of Freedom ...
    So What is a Mode Shape Anyway - Solving the Eigenvalue Problem
    • So What Is A Mode Shap...
    Forced Vibration of a SDOF System:
    • Forced Vibrations of a...
    Differential Equations Primer - Finding the Homogeneous (Transient) Solution:
    • Differential Equations...
    Differential Equations Primer - Finding the Particular (Steady-State) Solution:
    • Differential Equations...
    CHAPTERS:
    0:00 Intro
    0:52 Step-By-Step
    10:30 Recap
    11:30 Orthogonality of Normal Modes
    17:50 Example Problem
    22:46 Putting it All Together
    26:00 Outro

Комментарии • 25

  • @SLCMuralha
    @SLCMuralha Год назад +3

    Much appreciated! I only wish I had your videos when going through undergrad ME courses. It would have helped tremendously.

  • @BlackBox019
    @BlackBox019 Год назад +1

    Excellent video, thank you !!

  • @ibrahimhawraasafaaibrahimu3724

    you absolutely deserve a subscribe and a like and a share

  • @abhishekdixit23
    @abhishekdixit23 8 месяцев назад +1

    Thanx for such informative videos... Shows ur indepth knowledge about the subject...
    Binge watching ur content🎉

  • @ignatiusjacquesreilly70
    @ignatiusjacquesreilly70 Год назад +1

    Great video! If you have time I'd be interested in seeing this problem solved with proportional damping.

    • @Freeball99
      @Freeball99  Год назад +2

      Will have to make a video using proportional damping, but fundamentally this will just produce slight variations to the mass and stiffness matrices. The rest of the modeling will be the same.

  • @tryfonasthemas2220
    @tryfonasthemas2220 26 дней назад

    Is there any relationship of what you illustrated with the fourier transform? The steps we used remind me a lot of how one solves pdes in fourier space by converting them to odes.

  • @r2k314
    @r2k314 Год назад

    Thank you for the wonderfully clear step by step explanation. When I studied linear algebra, the inverse of the eigenvalue matrix was not it's transpose, so I have no Idea why the diagonalization worked. I'm glad it did, but I miss the point of the diagonalization, because you already have had to solve the system to do the diagonalization? I was hoping decoupling would lead to a way to construct arbitrary motion as a linear combination of the decoupled components.

    • @Freeball99
      @Freeball99  Год назад +1

      In order to perform the diagonalization, we need only solve the eigenvalue problem (ie we solve for the mode shapes - we do NOT solve the response problem). Once diagonalized, the equations are decoupled and exist in the form of n-independent equations each of which represents a simple harmonic oscillator (SHO). Because we readily know the solution to the SHO equations, we can write them (in terms of the normal coordinates). The actual response of the system can then easily be written as a linear combination of these normal coordinates.

    • @user-wx8bm1pg1d
      @user-wx8bm1pg1d 11 месяцев назад

      @@Freeball99 I'm still confused. Once we solve the eigenvalue problem, can't we just write x as a sum of the eigenvalues times a sinusoidal term of the corresponding frequency and be done with the problem? Also, all these matrix calculations seem like they would be computationally expensive. I still don't really see the point of this diagonalisation

  • @Itsgallon
    @Itsgallon Год назад

    Does the projection to modal coordinates still work to diagonalize mass and stiffness matrices in the solution of an aeroelastic system where aerodynamics are now introduced to the structural dynamics?

    • @Freeball99
      @Freeball99  Год назад +1

      Generally, the introduction of aerodynamic loads will add damping to the system that is non-proportional damping. In this case, the normal mode method will not work as is. However, it is still possible to use a modified version of the normal mode method that takes into account the effects of non-proportional damping. One such method is the modal analysis method, which requires solving the equations of motion with the aerodynamic loads included and then transforming the results into modal coordinates.

  • @christosgeorgiadis
    @christosgeorgiadis Год назад

    Could we use singular value decompostion (SVD) instead of eigenvalue decomposition that was used in this video? Do you know if this method is used in vibration problems. I'm curius. Thank you.

    • @Freeball99
      @Freeball99  Год назад +2

      Yes, certainly you could use other decompositions like SVD in vibrations problems. However, SVD is not as widely used as EVD in classical modal analysis, as EVD provides a more direct and straightforward way of obtaining the modal parameters of a system. However, SVD can still be a valuable tool in some vibration problems, especially when dealing with complex or non-square matrices, or when the goal is to extract the dominant patterns in the vibration data.

  • @nickgenin21
    @nickgenin21 8 месяцев назад

    professor, why not normalize it by the mass and get the [m] as diagonal 1 and the stiffness as omegai^2?

    • @Freeball99
      @Freeball99  8 месяцев назад

      You can do that. However, I find it easier (if doing it by hand) not to normalize the eigenvectors and then simply calculate the various omegas using the k's and m's from the diagonalized matrices...which is trivial.

  • @sdleakey
    @sdleakey Год назад

    Was just curious how this method still works when you don't include all of the eigenmodes of the system (as would be typical in FEA). I'm struggling to connect those math dots.

    • @Freeball99
      @Freeball99  Год назад

      All the modes have been included. This was done in eqn 3 where I wrote the response in terms of the normal coordinates and mode shapes: {x} = [Φ]·{η}. The modal matrix, [Φ], includes all the modes.

  • @Enggoat
    @Enggoat Год назад

    Please may you post the answer to the example problem in the comments or elsewhere, just to be able to check understanding of solving the problems?

    • @Freeball99
      @Freeball99  Год назад

      I don't have the solution for this because it is a problem I made up. You should be able to get there from the information in the video. I will need to create a separate video to explain this because I'm not going to be able to answer it in the comments.

  • @user-zx2tl4dl6e
    @user-zx2tl4dl6e 3 месяца назад

    What book are you referencing with this? Leonard meirovitch?

    • @Freeball99
      @Freeball99  3 месяца назад

      This comes from my class notes from years ago. Not sure what book the teacher used, but it certainly could have been Meirovich. However, I think that "Mechanical Vibrations" by Rao has a pretty good explanation of normal modes.

  • @tryfonasthemas2220
    @tryfonasthemas2220 26 дней назад

    Is there any relationship of what you illustrated with the fourier transform? The steps we used remind me a lot of how one solves pdes in fourier space by converting them to odes.

  • @tryfonasthemas2220
    @tryfonasthemas2220 26 дней назад

    Is there any relationship of what you illustrated with the fourier transform? The steps we used remind me a lot of how one solves pdes in fourier space by converting them to odes.

    • @Freeball99
      @Freeball99  16 дней назад

      Not really related. However, both allow one to extract the fundamental frequencies from the system, so they have that in common.
      In this particular video, we are dealing with ODEs and not a PDEs. We are using the normal mode method to decouple the equations of motions which allows us to easily solve each equation separately. We do this in the time domain. Fourier transform is used to transform a system from the time domain to the frequency domain.