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机译:涡轮增压固体推进剂冲压发动机的混合和燃烧增强
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Sichuan Aerosp Syst Engn Inst, Chengdu 610100, Sichuan, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Turbocharged Solid Propellant Ramjet; Numerical simulation; Mixing and combustion; Combustion efficiency; Specific impulse;
机译:涡轮增压固体推进剂冲压发动机的概念和性能研究
机译:通过数据科学方法开发固体推进剂燃烧的多因素计算模型。推进剂燃烧基因组观念
机译:油井条件下复合固体推进剂燃烧过程中高温气蒸气混合物处理近井筒的数学模型
机译:涡轮增压固体推进剂拉姆喷射的燃烧特性(TSPR)
机译:固体推进剂管道火箭发动机混合与燃烧过程的实验研究。
机译:单分散高能释放核/壳结构铝纳米粉的制备及其在HTPB推进剂中作为助燃剂的应用
机译:任意几何固体推进剂冲压发动机燃烧器高分散凝聚燃料燃烧效率对比分析方法