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- W2014705965 abstract "This paper introduces the FEA method for cyclic symmetric structures and makes an vibration characteristics analysis to a certain aeroengine compressor blade-disc coupling system based on this method. According to the anslysis results the dynamic characteristics of the blade-disc coupling system are discussed. The analysis method and results in this paper can be used for further study on optimal design and vibration safety verification for the blade-disc coupling system." @default.
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- W2014705965 date "2009-10-01" @default.
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- W2014705965 title "Vibration Analysis of Aeroengine Compressor Blade-Disc Coupling System" @default.
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- W2014705965 doi "https://doi.org/10.4028/www.scientific.net/amm.16-19.264" @default.
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