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The crack path in fuselage panel under mixed mode biaxial loading

Author(s):


Medium: journal article
Language(s): English
Published in: Frattura ed Integrità Strutturale, , n. 48, v. 13
Page(s): 87-96
DOI: 10.3221/igf-esis.48.11
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.48.11.
  • About this
    data sheet
  • Reference-ID
    10457701
  • Published on:
    24/10/2020
  • Last updated on:
    24/10/2020
 
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