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Optimal design of fighter aircraft wing panels laminates under multi-load case environment by ply-drop and ply-migrations

Author(s):


Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 207
Page(s): 909-922
DOI: 10.1016/j.compstruct.2018.09.004
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.2018.09.004.
  • About this
    data sheet
  • Reference-ID
    10449840
  • Published on:
    23/10/2020
  • Last updated on:
    23/10/2020
 
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