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Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model

Author(s): ORCID
ORCID
ORCID
ORCID
Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 352
Page(s): 118674
DOI: 10.1016/j.compstruct.2024.118674
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.2024.118674.
  • About this
    data sheet
  • Reference-ID
    10805768
  • Published on:
    10/11/2024
  • Last updated on:
    10/11/2024
 
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