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The computational post buckling analysis of fuselage stiffened panels loaded in compression

Author(s):



Medium: journal article
Language(s): English
Published in: Thin-Walled Structures, , n. 10, v. 42
Page(s): 1445-1464
DOI: 10.1016/j.tws.2004.04.002
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.tws.2004.04.002.
  • About this
    data sheet
  • Reference-ID
    10382086
  • Published on:
    23/11/2019
  • Last updated on:
    23/11/2019
 
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