Login
Register
Reset Password
Publish & Distribute
Publishing Solutions
Distribution Solutions
Subjects
Publications
Journals
Books
Proceedings
Publishers
Blog
Contact
Search
Cart
EUR
USD
GBP
English
English
Deutsch
Polski
Español
Français
Italiano
Home
Journals
Fatigue of Aircraft Structures
Volume 2017 (2017): Issue 9 (December 2017)
Open Access
Enhancement of Damage Detectability in Aircraft Structures Using the Fusion of NDT Results
Marcin Zapłotny
Marcin Zapłotny
,
Andrzej Katunin
Andrzej Katunin
and
Krzysztof Dragan
Krzysztof Dragan
| Aug 09, 2018
Fatigue of Aircraft Structures
Volume 2017 (2017): Issue 9 (December 2017)
About this article
Previous Article
Next Article
Abstract
References
Authors
Articles in this Issue
Preview
PDF
Cite
Share
Published Online:
Aug 09, 2018
Page range:
55 - 74
DOI:
https://doi.org/10.1515/fas-2017-0005
Keywords
aircraft composite structures
,
ultrasonic testing
,
information fusion
,
non-destructive testing
© 2017 Marcin Zapłotny et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.
Marcin Zapłotny
Institute of Fundamentals of Machinery Design, Silesian University of Technology
Gliwice, Poland
Andrzej Katunin
Institute of Fundamentals of Machinery Design, Silesian University of Technology
Gliwice, Poland
Krzysztof Dragan
Air Force Institute of Technology,
Warsaw, Poland