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Approach to Critical Crack Opening Displacement Modeling of Damage in Metal Sheets after Composite Patch Bonded Repair Cover

Approach to Critical Crack Opening Displacement Modeling of Damage in Metal Sheets after Composite Patch Bonded Repair

Fatigue of Aircraft Structures
Volume 2016 (2016): Issue 8 (June 2016)
By: Michał Sałacinski,  Andrzej Leski and  Michał Stefaniuk  
Open Access
|Jul 2017

Authors

Michał Sałacinski

michal.salacinski@itwl.pl

Air Force Institute of Technology, Warsaw, Poland

Andrzej Leski

andrzej.leski@wat.edu.pl

Military University of Technology, Faculty of Mechanical Engineering

Michał Stefaniuk

michal.stefaniuk@itwl.pl

Air Force Institute of Technology, Warsaw, Poland
DOI: https://doi.org/10.1515/fas-2016-0009 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 104 - 110
Published on: Jul 22, 2017
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
composites,
aerospace,
composite patch bonded repair
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2017 Michał Sałacinski, Andrzej Leski, Michał Stefaniuk, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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