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Design and analysis of adhesively bonded thick composite patch repair of corrosion grind-out and cracks on 2024 T3 clad aluminum aging aircraft structures

Author(s):

Medium: journal article
Language(s): English
Published in: Composite Structures, , n. 1-2, v. 76
Page(s): 138-150
DOI: 10.1016/j.compstruct.2006.06.020
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.2006.06.020.
  • About this
    data sheet
  • Reference-ID
    10461894
  • Published on:
    25/10/2020
  • Last updated on:
    25/10/2020
 
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