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Crack propagation monitoring in a full-scale aircraft fatigue test based on guided wave-Gaussian mixture model

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: 10.1088/0964-1726/25/5/055048.
  • About this
    data sheet
  • Reference-ID
    10226271
  • Published on:
    04/12/2018
  • Last updated on:
    04/12/2018
 
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