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Influence of modelling and solution methods on the FE-simulation of the post-buckling behaviour of stiffened aircraft fuselage panels

Author(s):


Medium: journal article
Language(s): English
Published in: Composite Structures, , n. 2, v. 73
Page(s): 229-236
DOI: 10.1016/j.compstruct.2005.11.048
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.2005.11.048.
  • About this
    data sheet
  • Reference-ID
    10461720
  • Published on:
    25/10/2020
  • Last updated on:
    25/10/2020
 
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