Estimation of Fatigue Properties of Composite Structures

Miroslaw Rodzewicz

doi:10.2478/v10164-010-0029-3

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Estimation of Fatigue Properties of Composite Structures

Fatigue of Aircraft Structures

Volume 2010 (2010): Issue 2 (December 2010)

By: Miroslaw Rodzewicz

Open Access

|Dec 2010

Abstract

The paper presents the proposal of a simplified method of fatigue properties estimation for polymer composite structures.

References

Rodzewicz, M. (2008). Determination and extrapolation of the glider load spectra. Aircraft Engineering and Aerospace Technology, 80(5), pp. 487-496.10.1108/00022660810899856
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Kensche, C., W. (2002). Proposal for a certification procedure of extended sailplane lifetime. Technical Soaring, 26(2), pp. 32-43.
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Rodzewicz, M. (2009). Fatigue evaluation of high-loaded aeronautical composite structures. Aircraft Engineering and Aerospace Technology, 81(5), pp. 452 - 460.10.1108/00022660910983743
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Articles in this issue

DOI: https://doi.org/10.2478/v10164-010-0029-3 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738

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Language: English

Page range: 87 - 97

Published online: Dec 20, 2010

Published in print: Dec 1, 2010

Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION

In partnership with: Paradigm Publishing Services

Related subjects:

Engineering,

Introductions and overviews,

Engineering, other

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

Volume 2010 (2010): Issue 2 (December 2010)