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Strength Testing and Analysis of Fatigue Crack Growth in Selected Aircraft Materials Cover

Strength Testing and Analysis of Fatigue Crack Growth in Selected Aircraft Materials

Fatigue of Aircraft Structures
Volume 2009 (2009): Issue 1 (July 2009)
By: Sylwester Kłysz and  Janusz Lisiecki  
Open Access
|Sep 2010

References

  1. American Society fot Testing and Materials. (2004). Standard Practice for Strain-Controlled Testing. E 606. West Conshonocken, PA: ASTM International. (DOI 10.1520/E0606-04E01)
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  2. PN-ISO (1996) Metals - Sheets and Tapes - Determination of Tensile Strain-Hardening Exponent. 10275. Polish Committee for Standardization, Warsaw, Poland.
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DOI: https://doi.org/10.2478/v10164-010-0008-8 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 74 - 83
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 Sylwester Kłysz, Janusz Lisiecki, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

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