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Stress/strain tensor for anisotropic materials

  1. Apr 13, 2016 #1

    I understand stress, strain but when it moves on to 3 dimension anisotropic materials using tensors and stiffness matrices I get confused with einstein's notation. can someone please help me out in this regard to undrstand how stiffness and compliance matrices get reduced for monoclinic, orthotropic materials?
  2. jcsd
  3. Apr 14, 2016 #2
    Are you trying to do it for a stack of uni's?
  4. Apr 14, 2016 #3
    i wan to start off with a stack of uni's and then move on to bi-directionals. The main problem is i am unable to visualise einstein's notation and to differentiate when it is that and when it is not.
  5. Apr 14, 2016 #4
    This is einstein's summation convention?
  6. Apr 14, 2016 #5
  7. Apr 14, 2016 #6
    Please tell us what your understanding of the einstein summation convention is so that we can better pinpoint what your difficulty is.
  8. Apr 14, 2016 #7
    Ok einstein summation is that for when an index is being repeated in the forumlation for example a11+a12/SUB]+a13+a14 then it can be written as aij j=1,2,3 and also for orthotropic materials the compliance/stiffness matrix reduces to 21 constants. Can someone please explain how??
    Last edited: Apr 14, 2016
  9. Apr 14, 2016 #8
    That's not the Einstein summation convention. The Einstein convention says that, if an index is repeated in an expression, summation over that index is implied. It's the same as if you had a summation sign in front of the expression. The Einstein summation convention is typically used in stress-strain contexts to concisely represent matrix multiplication (without having to include the summation sign). An example is aijbjk.
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