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

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
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 on: Aug 25, 2011
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
compressor blade,
damage,
fatigue,
modal analysis,
lattice-spin coupling,
FEM
Related subjects:
Engineering,
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)