Hits:
Date of Publication:2022-10-07
Journal:International Journal of Aerospace Engineering
Affiliation of Author(s):运载工程与力学学部
Volume:2019
ISSN No.:1687-5966
Pre One:超声波测量固体推进剂燃速的关键技术
Next One:Numerical simulation of the start process of a han-based mono-propellant rocket thruster
