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  1. cgcg1

    Dear friends FEM FEMAP HONEYCOMB CO

    To Clarify, I meant, "Shear Modulus values of “2z” and “1z” respectively, that were entered in the “2D Orthotropic” material Tab in Femap. Thank you very much and looking forward to hear from you" are for the CORE Material only. As for the Face sheet layers, they are "isotropic Aluminum...
  2. cgcg1

    Dear friends FEM FEMAP HONEYCOMB CO

    Thank you very much Blas, sorry for late reply I am new in this forum website took me a while to find out how I reply to you to thank you. I visited your website it was excellent. Correct me if if I’m wrong, the way I understand it the “Lam Ply YZ Shear Stress” and “Lam Ply XZ Shear Stress”...
  3. cgcg1

    Dear friends FEM FEMAP HONEYCOMB CO

    Dear friends FEM FEMAP HONEYCOMB CORE I have a question about filling up the Material property Tab in Femap. Let’s say we have honeycomb aluminum core sandwiched between the two thin aluminum face sheets. I understand that the core material in a honeycomb sandwich panel can be modeled as a...
  4. cgcg1

    Dear friends I have a question a

    Dear friends I have a question about filling up the Material property Tab in Femap. Let’s say we have honeycomb aluminum core sandwiched between the two thin aluminum face sheets. I understand that the core material in a honeycomb sandwich panel can be modeled as a 2D-Orthotropic Material...
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