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Simulating Crack Propagation of a Selected Structural Component of the PZL-130 Orlik TC-II Aircrafts Cover

Simulating Crack Propagation of a Selected Structural Component of the PZL-130 Orlik TC-II Aircrafts

Fatigue of Aircraft Structures
Volume 2014 (2014): Issue 6 (June 2014)
By:  and    
Open Access
|Jun 2015
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DOI: https://doi.org/10.1515/fas-2014-0013 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 119 - 127
Published online: Jun 30, 2015
Published in print: Jun 1, 2014
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Keywords:
structural integrity,
crack propagation simulation,
geometry correction factor
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2015 Krzysztof Jankowski, Piotr Reymer, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Volume 2014 (2014): Issue 6 (June 2014)
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