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Analytical studies and numerical predictions of stresses in shear joints of layered composite panels for aerospace applications

Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.1016/j.compstruct.2020.112927.
  • About this
    data sheet
  • Reference-ID
    10447220
  • Published on:
    23/10/2020
  • Last updated on:
    23/10/2020
 
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