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How to calculate Young's modulus of layered cross section

  1. Aug 13, 2015 #1
    Given a rectangular prism that is composed of various horizontal layers made of different materials, how can one calculate the modulus of elasticity? Currently the materials used and their respective ratios have not been specified. We wish to determine this information using the results of trying to find the modulus.
     
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  3. Aug 13, 2015 #2

    Nidum

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    If in the end you want to work out stresses and deflections a piecewise method is needed using the individual Young's moduli of the different layers .
     
  4. Aug 13, 2015 #3

    SteamKing

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    It depends on what you are trying to accomplish.

    If you want to calculate the bending stresses in a beam made of this layered material, there is a way to calculate a weighted-modulus if you know the moduli of the individual components.

    Other than this, we'll need further information.
     
  5. Aug 13, 2015 #4
    The end goal is to calculate the buckling load of the overall material. Given a specific list of materials and their elastic moduli, is it possible to mathematically set up a process to find the modulus of the overall structure?

    I have looked into the Rule of Mixtures, but I am not sure if it is applicable here.
     
  6. Aug 13, 2015 #5

    Nidum

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    An expression can be derived for a beam of specific dimensions and layer construction but there are difficulties in arriving at a truly meaningful value .

    In a laminated beam the strength and flexibility of the bond between layers has to be included .
     
  7. Aug 14, 2015 #6
    Could someone please elaborate on the procedure and how someone should go about it?
     
  8. Aug 14, 2015 #7
    You assume that, since all the layers are glued together, they all experience the same in-plane strain. Once you know the strains, you can calculate the stresses in each layer, and average these to get the average modulii. If it is a uniaxial unconstrained deformation, you first solve for the strain that makes the average transverse stress zero, and then determine the average axial stress.

    Information like this should be available in the Composite literature.

    Chet
     
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