Systematic multiparameter design methodology for an ultrasonic health monitoring system for full‐scale composite aircraft primary structures-Reference-Cited by-同舟云学术

Systematic multiparameter design methodology for an ultrasonic health monitoring system for full‐scale composite aircraft primary structures

Published:2019-02-21 Issue:5 Volume:26 Page:e2340
ISSN:1545-2255
Container-title:Structural Control and Health Monitoring
language:en
Short-container-title:Struct Control Health Monit

Author:

Ochôa Pedro¹²^ORCID,Groves Roger M.²^ORCID,Benedictus Rinze¹

Affiliation:

1. Structural Integrity and Composites Group, Faculty of Aerospace EngineeringDelft University of Technology Delft The Netherlands

2. Aerospace Non‐Destructive Testing Laboratory, Faculty of Aerospace EngineeringDelft University of Technology Delft The Netherlands

Funder

Netherlands Enterprise Agency of the Ministry of Economic Affairs

Publisher

Wiley

Subject

Mechanics of Materials,Building and Construction,Civil and Structural Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/stc.2340

Reference44 articles.

1. WenkL BockenheimerC.Structural health monitoring: a real‐time on board ‘stethoscope’ for condition‐based maintenance. Airbus Technical Magazine ‐ Flight Airworthiness Support Technology. August 2014: 22.

2. GardinerG.Structural health monitoring: NDT‐integrated aerostructures enter service.Composites World31 July 2015.https://www.compositesworld.com/articles/structural‐health‐monitoring‐ndt‐integrated‐aerostructures‐enter‐service. Accessed July 25 2018.

3. Guided Lamb waves for identification of damage in composite structures: A review

4. Identification of Damage Using Lamb Waves

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