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

Sylwester Kłysz; Janusz Lisiecki

doi:10.2478/v10164-010-0008-8

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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

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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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

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© 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)