Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring

Vincentius Ewald, Roger M. Groves, Rinze Benedictus

Open source

DOI: 10.3390/aerospace5020039
Published: 2018-04-04
Container: Aerospace
Publisher: MDPI AG
Open access: unknown

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Cite this work

BibTeX

@article{allodium:10.3390/aerospace5020039,
  title = {Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring},
  author = {Vincentius Ewald and Roger M. Groves and Rinze Benedictus},
  year = {2018},
  journal = {Aerospace},
  doi = {10.3390/aerospace5020039},
  url = {https://doi.org/10.3390/aerospace5020039}
}

RIS

TY  - JOUR
TI  - Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring
AU  - Vincentius Ewald
AU  - Roger M. Groves
AU  - Rinze Benedictus
PY  - 2018
JO  - Aerospace
DO  - 10.3390/aerospace5020039
UR  - https://doi.org/10.3390/aerospace5020039
ER  -

APA

Ewald, V., Groves, R. M., & Benedictus, R. (2018). Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring. Aerospace. https://doi.org/10.3390/aerospace5020039

Source records

crossref · retrieved 2026-09-24T19:27:28.850Z