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A refined aeroelastic beam finite element for the stability analysis of flexible subsonic wings

Author(s): ORCID




Medium: journal article
Language(s): English
Published in: Computers & Structures, , v. 307
Page(s): 107618
DOI: 10.1016/j.compstruc.2024.107618
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.compstruc.2024.107618.
  • About this
    data sheet
  • Reference-ID
    10809447
  • Published on:
    07/01/2025
  • Last updated on:
    07/01/2025
 
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