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Explosive blast loading effect on transient mechanical responses of aircraft panels with curvilinear fibers: 3D elasticity approach

Author(s):


Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 334
Page(s): 117967
DOI: 10.1016/j.compstruct.2024.117967
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.2024.117967.
  • About this
    data sheet
  • Reference-ID
    10775012
  • Published on:
    29/04/2024
  • Last updated on:
    29/04/2024
 
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