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Published in 2019 at "Journal of Vibroengineering"
DOI: 10.21595/jve.2019.20740
Abstract: This paper presents a method of mistuning identification of a random mistuned bladed parameter, to predict the forced vibration characteristics of random mistuned blade disk of aeroengine compressor, based on the prestress mode synthesis method,…
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Keywords:
blade disk;
disk;
mistuned bladed;
random mistuned ... See more keywords