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Influence of the Fatigue Load Level and the Hole Diameter on the Laminate Structure’s Fatigue Performance Cover

Influence of the Fatigue Load Level and the Hole Diameter on the Laminate Structure’s Fatigue Performance

Fatigue of Aircraft Structures
Volume 2018 (2018): Issue 10 (December 2018)
By: Małgorzata Zalewska  
Open Access
|Jun 2019

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DOI: https://doi.org/10.2478/fas-2018-0002 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 21 - 30
Published on: Jun 28, 2019
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
composite,
fatigue,
damage
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2019 Małgorzata Zalewska, 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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