Acoustic-instability boundaries in liquid-propellant rockets: Theoretical explanation of empirical correlation

被引:19
作者
Kim, JS
Williams, FA
机构
[1] University of California, San Diego, San Diego
[2] Dept. Eng. Physics Combustion, Ctr. for Ener. and Combust. Research
关键词
D O I
10.2514/3.24081
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:621 / 624
页数:4
相关论文
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