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Inspection interval optimization of aircraft landing gear component based on risk assessment using equivalent initial flaw size distribution method

Author(s): (Aero Technology Research Institute, Daegu, Korea)
(Aero Technology Research Institute, Daegu, Korea)
ORCID (Department of Defense Science, Korea National Defense University, Nonsan, Korea)
Medium: journal article
Language(s): English
Published in: Structural Health Monitoring, , n. 4, v. 21
Page(s): 147592172110336
DOI: 10.1177/14759217211033625
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: 10.1177/14759217211033625.
  • About this
    data sheet
  • Reference-ID
    10627276
  • Published on:
    05/09/2021
  • Last updated on:
    20/06/2022
 
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