First-order approximate rigid-flexible coupled dynamics analysis of a simple aero-engine blade model with dynamic stiffening effect
Crossref DOI link: https://doi.org/10.1007/s12206-021-0623-z
Published Online: 2021-06-29
Published Print: 2021-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Wei, Zhe
Li, Li
Zhao, Fang
Text and Data Mining valid from 2021-06-29
Version of Record valid from 2021-06-29
Article History
Received: 6 May 2020
Revised: 28 January 2021
Accepted: 30 March 2021
First Online: 29 June 2021