Surface Profiling and Core Evaluation of Aluminum Honeycomb Sandwich Aircraft Panels Using Multi-Frequency Eddy Current Testing.

Reyno T, Underhill PR, Krause TW, Marsden C, Wowk D

DOI: 10.3390/s17092114
Published: 2017 Sep 14
Container: Sensors (Basel, Switzerland)
Publisher: Not recorded
Open access: yes

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Cite this work

BibTeX

@article{allodium:10.3390/s17092114,
  title = {Surface Profiling and Core Evaluation of Aluminum Honeycomb Sandwich Aircraft Panels Using Multi-Frequency Eddy Current Testing.},
  author = {Reyno T and Underhill PR and Krause TW and Marsden C and Wowk D},
  year = {2017},
  journal = {Sensors (Basel, Switzerland)},
  doi = {10.3390/s17092114},
  url = {https://doi.org/10.3390/s17092114}
}

RIS

TY  - JOUR
TI  - Surface Profiling and Core Evaluation of Aluminum Honeycomb Sandwich Aircraft Panels Using Multi-Frequency Eddy Current Testing.
AU  - Reyno T
AU  - Underhill PR
AU  - Krause TW
AU  - Marsden C
AU  - Wowk D
PY  - 2017
JO  - Sensors (Basel, Switzerland)
DO  - 10.3390/s17092114
UR  - https://doi.org/10.3390/s17092114
ER  -

APA

T, R., PR, U., TW, K., C, M., & D, W. (2017). Surface Profiling and Core Evaluation of Aluminum Honeycomb Sandwich Aircraft Panels Using Multi-Frequency Eddy Current Testing.. Sensors (Basel, Switzerland). https://doi.org/10.3390/s17092114

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pubmed · retrieved 2026-09-24T19:48:13.612Z