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Compressor Blade Fatigue Diagnostics and Modelling with the Use of Modal Analysis Cover

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Compressor Blade Fatigue Diagnostics and Modelling with the Use of Modal Analysis

Fatigue of Aircraft Structures

Volume 2011 (2011): Issue 3 (August 2011)

By: Mirosław Witoś and Michał Stefaniuk

Open Access

|Aug 2011

Articles in this issue

DOI: https://doi.org/10.2478/v10164-010-0044-4 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738

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Language: English

Page range: 112 - 133

Published online: Aug 25, 2011

Published in print: Aug 1, 2011

Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION

In partnership with: Paradigm Publishing Services

Keywords:

compressor blade,

modal analysis,

lattice-spin coupling,

Related subjects:

Introductions and overviews,

Engineering, other

© 2011 Mirosław Witoś, Michał Stefaniuk, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2011 (2011): Issue 3 (August 2011)

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