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The effect of flexural/twist anisotropy on compression buckling of quasi-isotropic laminated cylindrical shells

Author(s):


Medium: journal article
Language(s): English
Published in: Composite Structures, , n. 2, v. 55
Page(s): 195-204
DOI: 10.1016/s0263-8223(01)00147-7
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(01)00147-7.
  • About this
    data sheet
  • Reference-ID
    10460789
  • Published on:
    25/10/2020
  • Last updated on:
    25/10/2020
 
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