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On-line updating Gaussian mixture model for aircraft wing spar damage evaluation under time-varying boundary condition

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: 10.1088/0964-1726/23/12/125001.
  • About this
    data sheet
  • Reference-ID
    10225676
  • Published on:
    04/12/2018
  • Last updated on:
    04/12/2018
 
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