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Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin Cover

Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin

Fatigue of Aircraft Structures
Volume 2009 (2009): Issue 1 (July 2009)
By: Petr Augustin  
Open Access
|Sep 2010
DOI: https://doi.org/10.2478/v10164-010-0001-2 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 5 - 19
Published on: Sep 23, 2010
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

© 2010 Petr Augustin, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2009 (2009): Issue 1 (July 2009)