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Finite element model updating of a satellite honeycomb sandwich plate in structural dynamics

Author(s): ORCID (Aircraft Mechanics Department, Military Technical College, Cairo, Egypt)
(Aircraft Mechanics Department, Military Technical College, Cairo, Egypt)
(Aircraft Mechanics Department, Military Technical College, Cairo, Egypt)
(Aircraft Mechanics Department, Military Technical College, Cairo, Egypt)
Medium: journal article
Language(s): English
Published in: International Journal of Space Structures, , n. 2, v. 36
Page(s): 095605992110016
DOI: 10.1177/09560599211001683
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: 10.1177/09560599211001683.
  • About this
    data sheet
  • Reference-ID
    10603641
  • Published on:
    17/04/2021
  • Last updated on:
    29/06/2021
 
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