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Damage tolerance allowable calculation for the aircraft design with static ultimate load

Author(s):

ORCID


Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 329
Page(s): 117803
DOI: 10.1016/j.compstruct.2023.117803
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.2023.117803.
  • About this
    data sheet
  • Reference-ID
    10755327
  • Published on:
    14/01/2024
  • Last updated on:
    14/01/2024
 
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