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The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel

Author(s):



Medium: journal article
Language(s): English
Published in: Frattura ed Integrità Strutturale, , n. 50, v. 13
Page(s): 126-140
DOI: 10.3221/igf-esis.50.12
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: 10.3221/igf-esis.50.12.
  • About this
    data sheet
  • Reference-ID
    10457420
  • Published on:
    24/10/2020
  • Last updated on:
    24/10/2020
 
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