The effort of spray characteristic on rocket engine combustion stability for hypergolic propellant (MMH/NTO) was studied.

 
  • 用数值方法研究了一甲基肼/四氧化二氮自燃推进剂(MMH/NTO)喷雾液滴直径对火箭发动机燃烧稳定性的影响。
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