Funding for this research was provided by:
National Natural Science Foundation of China (51675266)
the Aeronautical Science Foundation of China (2014ZB52024)
Postgraduate Research & Practice Innovation Program of Jiangsu Province (KYCX18_0314)
the Fundamental Research Funds for the Central Universities (NJ20160038)
the Jiangsu Province Key Laboratory of Aerospace Power System (CEPE2019004)
Article History
Received: 31 July 2019
Accepted: 26 November 2019
First Online: 9 December 2019