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A general solution for stresses around holes in symmetric laminates under inplane loading

Author(s):

Medium: journal article
Language(s): English
Published in: Composite Structures, , n. 3, v. 49
Page(s): 339-354
DOI: 10.1016/s0263-8223(00)00070-2
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/s0263-8223(00)00070-2.
  • About this
    data sheet
  • Reference-ID
    10460504
  • Published on:
    25/10/2020
  • Last updated on:
    25/10/2020
 
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