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Nonlinear thermal flutter analysis of variable angle tow composite curved panels in supersonic airflow

Author(s):

Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 277
Page(s): 114610
DOI: 10.1016/j.compstruct.2021.114610
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.2021.114610.
  • About this
    data sheet
  • Reference-ID
    10631604
  • Published on:
    01/10/2021
  • Last updated on:
    01/10/2021
 
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