Hey all, here's the deets.

I'm using an L beam depicted in the first picture, with t/b at 0.01, 0.02, 0.03, 0.04 and the other dimensions as shown, poisson at 0.35.

Here's the steps I took in abaqus:

  • Import the ACIS part from solidworks (scale to 0.001 on import to convert mm to m)
  • Assign the section and material (74.5E9 for Young's, 0.35 poisson)
  • Add a "Linear Perturbation - Buckling" step
  • Add two reference points at the centroid of the part, at opposite ends, based on the location given in the excel file
  • Set up a "Constraint - Coupling", kinematic type with U1 U2 U3 and UR1 UR2 UR3 constrained for both reference points
  • Set BC on one reference point at the "Initial Step" to U1 U2 U3
  • Set BC on the other reference point at the "Initial Step" to U2 U3 (beam is laying on the X axis)
  • Add a "Load - Concentrated Force" equal to "-1" on the CF1 dimension on the "Buckle" step with the point load applied to the Reference Point and the loaded end
  • Mesh the part in the assembly level
  • Run the job
  • At this point, the solution I obtain in abaqus has been 20% below the book values, or more. This can be seen in the excel file.

    I need to confirm that the way I'm setting up the model corresponds with the real world, so that I can proceed with my research knowing that my control setup is accurate, as I will be using orthotropic instead of isotropic materials.

    Any ideas on what I could be doing wrong? I'm including both the excel file that has information on the control results, and the .SAT files I used to create the models in Abaqus. I attempted to upload the .CAE or the .ODB files, but no luck on ResearchGate.

    Help please!

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