Login
Register
Reset Password
Publish & Distribute
Publishing Solutions
Distribution Solutions
Subjects
Architecture and Design
Arts
Business and Economics
Chemistry
Classical and Ancient Near Eastern Studies
Computer Sciences
Cultural Studies
Engineering
General Interest
Geosciences
History
Industrial Chemistry
Jewish Studies
Law
Library and Information Science, Book Studies
Life Sciences
Linguistics and Semiotics
Literary Studies
Materials Sciences
Mathematics
Medicine
Music
Pharmacy
Philosophy
Physics
Social Sciences
Sports and Recreation
Theology and Religion
Publications
Journals
Books
Proceedings
Publishers
Blog
Contact
Search
EUR
USD
GBP
English
English
Deutsch
Polski
Español
Français
Italiano
Cart
Home
Journals
Fatigue of Aircraft Structures
Volume 2018 (2018): Issue 10 (December 2018)
Open Access
Influence of the Fatigue Load Level and the Hole Diameter on the Laminate Structure’s Fatigue Performance
Małgorzata Zalewska
Małgorzata Zalewska
| Jun 28, 2019
Fatigue of Aircraft Structures
Volume 2018 (2018): Issue 10 (December 2018)
About this article
Previous Article
Next Article
Abstract
References
Authors
Articles in this Issue
Preview
PDF
Cite
Share
Published Online:
Jun 28, 2019
Page range:
21 - 30
DOI:
https://doi.org/10.2478/fas-2018-0002
Keywords
composite
,
fatigue
,
damage
© 2019 Małgorzata Zalewska, published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.
Małgorzata Zalewska
Institute of Aviation
Warsaw, Poland