Funding for this research was provided by:
the National Natural Science Foundation of China granted (No. 51505070, No. 51970530 and U1708257)
the Fundamental Research Funds for the Central Universities of China granted (No. N160313002, N160312001, N170302001 and N180313006)
the Scholarship Fund of China Scholarship Council (CSC) granted (No. 201806085032)
the Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University, granted (No.VCAME201603)
Article History
Received: 23 April 2019
Accepted: 4 May 2020
First Online: 22 June 2020
Compliance with Ethical Standards
:
: The authors declare no potential conflicts of interest with respect to the research, authorship, and/or publication of this article.