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Uncertainty quantification in the modal analysis of aircraft stiffeners: A Perturbation Technique approach in SFEM

Author(s):


Medium: journal article
Language(s): English
Published in: Engineering Structures, , v. 323
Page(s): 119187
DOI: 10.1016/j.engstruct.2024.119187
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.engstruct.2024.119187.
  • About this
    data sheet
  • Reference-ID
    10801673
  • Published on:
    10/11/2024
  • Last updated on:
    10/11/2024
 
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