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机译:具有轻微温度升高燃烧的氢双旋燃机结构特性的数值研究
Beihang Univ Sch Energy & Power Engn Xueyuan Rd Beijing 100191 Peoples R China;
Beihang Univ Sch Energy & Power Engn Xueyuan Rd Beijing 100191 Peoples R China;
Beihang Univ Sch Energy & Power Engn Xueyuan Rd Beijing 100191 Peoples R China|Beihang Univ Res Inst Aeroengine Xueyuan Rd Beijing 100191 Peoples R China;
Beihang Univ Sch Energy & Power Engn Xueyuan Rd Beijing 100191 Peoples R China|Beihang Univ Res Inst Aeroengine Xueyuan Rd Beijing 100191 Peoples R China;
Aero Engine Grp Corp China Aero Engine Acad China Beijing 101304 Peoples R China;
Beihang Univ Sch Energy & Power Engn Xueyuan Rd Beijing 100191 Peoples R China;
Gas turbine; Swirler; Combustion; Gaseous fuel combustion; Hydrogen;
机译:喷射方式对带腔燃气轮机燃烧室温升燃烧特性的影响
机译:注射模式对汽轮机燃烧器轻微温度升高燃烧燃烧特性的影响
机译:燃气轮机涡流燃烧器内温升燃烧的实验研究
机译:Onera-LAERTE设施的LAPCAT-Ⅱ双模Ramjet燃烧室中热气流中氢的燃烧-实验和数值研究
机译:燃烧不稳定性:贫油预混燃烧器中氢气影响的实验研究。
机译:填充床中N2稀释的CH4和O2扩散燃烧燃烧特性的实验和数值研究
机译:基于乙烯反应机理的波转子燃烧器燃烧特性的数值研究
机译:双涡流燃烧室一次区流场,成分和温度的激光诊断测量。