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Normal stress flow evaluation in composite aircraft wing sections by strength of material models

Author(s):

Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 282
Page(s): 115088
DOI: 10.1016/j.compstruct.2021.115088
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.2021.115088.
  • About this
    data sheet
  • Reference-ID
    10647242
  • Published on:
    07/01/2022
  • Last updated on:
    07/01/2022
 
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