Analytical modeling of the coupled nonlinear free vibration response of a rotating blade in a gas turbine engine
Crossref DOI link: https://doi.org/10.1007/s00707-018-2165-8
Published Online: 2018-05-17
Published Print: 2018-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Roy, P. A.
Meguid, S. A.
Funding for this research was provided by:
Natural Sciences and Engineering Research Council of Canada (48568/2013-2017)
Text and Data Mining valid from 2018-05-17
Article History
Received: 21 November 2017
Revised: 13 February 2018
First Online: 17 May 2018