Wang, Lei
Liu, Yaru
Funding for this research was provided by:
Pre-research Field Foundation of Equipment Development Department of China (61402100103)
Aeronautical Science Foundation of China (2017ZA51012; 20182951014)
Defense Industrial Technology Development Program (JCKY2016204B101, JCKY2017208B001)
Industrial Corporation and the College Union Innovation Foundation of China Academy of Launch Vehicle Technology (CALT201704)
Article History
Received: 25 July 2019
Revised: 30 September 2019
Accepted: 3 November 2019
First Online: 31 January 2020
Compliance with ethical standards
:
: On behalf of the authors, the corresponding author states that there is no conflict of interest.