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Embedded fiber Bragg grating sensor–based wing load monitoring system for composite aircraft

Author(s):



Medium: journal article
Language(s): English
Published in: Structural Health Monitoring, , n. 4, v. 18
Page(s): 1337-1351
DOI: 10.1177/1475921719843772
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: 10.1177/1475921719843772.
  • About this
    data sheet
  • Reference-ID
    10562293
  • Published on:
    11/02/2021
  • Last updated on:
    19/02/2021
 
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