Funding for this research was provided by:
National Natural Science Foundation of China (No. 51505070)
the Fundamental Research Funds for the Central Universities of China (No. N160313002, N160312001, N170302001, N180413004)
the Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University (No.VCAME201603)
Article History
Received: 14 April 2019
Accepted: 3 December 2019
First Online: 19 December 2019
Compliance with ethical standards
:
: The authors declare that there is no conflict of interests regarding the publication of this paper.