Numerical analysis on thermal environment of liquid rocket with afterburning under different altitudes

标题
Numerical analysis on thermal environment of liquid rocket with afterburning under different altitudes
作者
关键词
Afterburning effect, Thermal environment, Chemical mechanism, LH, 2, /LOX rocket, Numerical simulation
出版物
APPLIED THERMAL ENGINEERING
Volume 178, Issue -, Pages 115584
出版商
Elsevier BV
发表日期
2020-06-12
DOI
10.1016/j.applthermaleng.2020.115584

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