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15-Moonstone
May 14, 2014
Question

Explanation of Buckling

  • May 14, 2014
  • 2 replies
  • 7679 views

Hello,
Someone he already made simulations of buckling.
Because I do not understand the result in buckling of a rod with several ( BLF) bending load factor , I still get
the same scale of displacement, with a maximum displacement of 1 [mm] .
I made several simulations of various shapes and load and I have always the same result, a displacement of 1 [mm] .

To view the buckling, we have to go through a static simulation model with all the stress conditions and charges
before proceeding to the simulation of buckling which includes the previous results of the static simulation.
Where I think the actual load must be important.

In the knowledge base PTC it is written :
For the stresses and displacements of the structure at the critical buckling load , the greater the BLF must be multiplied
by the initial compression load used in the static analysis . The initial load shall be changed
this value and static analysis restarted. Pro / SIMULATE not calculate the stresses due to buckling ,
because it is the field of nonlinear large deformation calculations .

If you have an idea , it will be welcome or a sample file .
Cordially.
Denis .


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2 replies

13-Aquamarine
May 14, 2014

Hi Denis,

A partial answer for you.

BLF= Buckling Load Factor

I believe the modal solver is used to calculate the buckling mode shapes. These mode shapes (eigen vectors) are normalised to amplitude 1.

Multiply the load applied in the initial static analysis by the BLF to get the load at which buckling will occur.

Regards

Charles

15-Moonstone
May 14, 2014

Hello, Charles,

Thank you for the very quick response, I'll see what happens.

Cordially.

Denis.

2-Explorer
May 14, 2014

As Charles pointed out, the buckling analysis in Creo Simulate (Pro/Mechanica) is solving an eigenvalue problem (same as a modal analysis), where your eigenvalues are the Buckling Load Factors (the factor of the applied load "needed" to cause buckling) and the eigenvectors are the buckling mode shape. For an eigenvalue problem, Mechanica will always normalize the results (i.e. the largest "displacement" is 1).

Now, all that being said, it's very important to keep in mind that last sentence from the knowledge base: "Pro / SIMULATE not calculate the stresses due to buckling, because it is the field of nonlinear large deformation calculations."

The analysis you're doing is sometimes called a linear bucking analysis, because the solution is a linear perturbation of the intial change in the structures stiffness due to the base static analysis. There are two very important points about a linear buckling analysis that must be kept in mind:

  1. There is a unknown amount of error between the linear and non-linear buckling solution.
  2. The linear buckling solution is unconservative (i.e. the calculated buckling load is higher than the true buckling load).

https://forum.solidworks.com/servlet/JiveServlet/downloadImage/2-415724-124547/450-374/Buckling.PNG

The implication of these two points (particularly the last one) means that you need to be very careful how you use the results from a linear buckling analysis. Realistically, a linear buckling analysis should only be used for preliminary comparisons (what type of buckling mode could exist, and how design changes effect the trend of the BLF). If the results are used for anything else, then a high factor of safety is needed. More accurate results can be obtained by running a non-linear analysis with large-displacement formulation and a non-linear material property. If you do this, be sure to include some eccentricity in your model (whether load or geometric).

15-Moonstone
May 14, 2014

Hello, Shaun,

Thank you to you for this very interesting explanation.

I'll take it all.

Cordially.

Denis.