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The Analysis of Fatigue Crack Propagation in the Elements of Aluminum Alloy D16CZATW with a Notch in the Formof A Cylindrical Hole Cover

The Analysis of Fatigue Crack Propagation in the Elements of Aluminum Alloy D16CZATW with a Notch in the Formof A Cylindrical Hole

Fatigue of Aircraft Structures
Volume 2011 (2011): Issue 3 (August 2011)
By: Volodymyr Hutsaylyuk,  Janusz Mierzyński and  Dariusz Zasada  
Open Access
|Aug 2011

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DOI: https://doi.org/10.2478/v10164-010-0035-5 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 28 - 41
Published on: Aug 25, 2011
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2011 Volodymyr Hutsaylyuk, Janusz Mierzyński, Dariusz Zasada, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2011 (2011): Issue 3 (August 2011)