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Aeroelastic tailoring method of tow-steered composite wing using matrix perturbation theory

Author(s):


Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 234
Page(s): 111696
DOI: 10.1016/j.compstruct.2019.111696
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.2019.111696.
  • About this
    data sheet
  • Reference-ID
    10448434
  • Published on:
    23/10/2020
  • Last updated on:
    23/10/2020
 
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