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Fatigue of Aircraft Structures
Volume 2011 (2011): Issue 3 (August 2011)
Open Access
Compressor Blade Fatigue Diagnostics and Modelling with the Use of Modal Analysis
Mirosław Witoś
Mirosław Witoś
and
Michał Stefaniuk
Michał Stefaniuk
| Aug 25, 2011
Fatigue of Aircraft Structures
Volume 2011 (2011): Issue 3 (August 2011)
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Published Online:
Aug 25, 2011
Page range:
112 - 133
DOI:
https://doi.org/10.2478/v10164-010-0044-4
Keywords
compressor blade
,
damage
,
fatigue
,
modal analysis
,
lattice-spin coupling
,
FEM
This content is open access.