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Maximum buckling loads for unsymmetric thin hybrid laminates under in-plane and shear forces

Author(s):

Medium: journal article
Language(s): English
Published in: Composite Structures, , n. 1-2, v. 36
Page(s): 1-11
DOI: 10.1016/s0263-8223(96)00047-5
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(96)00047-5.
  • About this
    data sheet
  • Reference-ID
    10459999
  • Published on:
    25/10/2020
  • Last updated on:
    25/10/2020
 
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