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Through-the-thickness stress distributions near edges of composite laminates using stress recovery scheme and third order shear and normal deformable theory

Author(s):

Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 131
Page(s): 397-413
DOI: 10.1016/j.compstruct.2015.05.041
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.2015.05.041.
  • About this
    data sheet
  • Reference-ID
    10453637
  • Published on:
    23/10/2020
  • Last updated on:
    23/10/2020
 
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