![](/img/cover-not-exists.png)
Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement
Youyin, Wang, Kunlin, Cheng, Jingfeng, Tang, Xiaoyong, Liu, Wen, BaoLanguage:
english
Journal:
Aerospace Science and Technology
DOI:
10.1016/j.ast.2019.105594
Date:
November, 2019
File:
PDF, 771 KB
english, 2019