机译:燃气轮机涡流燃烧器内温升燃烧的实验研究
Beijing Univ Aeronaut & Astronaut, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengines Aerothermo, Beijing 100191, Peoples R China;
Beijing Univ Aeronaut & Astronaut, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengines Aerothermo, Beijing 100191, Peoples R China;
Xiamen Univ, Sch Phys & Mech & Elect Engn, Xiamen 361005, Fujian, Peoples R China;
Aviat Ind Corp China, China Aviat Powerplant Res Inst, Zhuzhou 412002, Hunan, Peoples R China;
Beijing Univ Aeronaut & Astronaut, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengines Aerothermo, Beijing 100191, Peoples R China;
Univ Surrey, Fac Engn & Phys Sci, Dept Mech Engn Sci, Guildford GU2 7XH, Surrey, England;
Beijing Univ Aeronaut & Astronaut, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengines Aerothermo, Beijing 100191, Peoples R China;
Combustion; Vortex; Cavity; Kerosene; Experiment; Evaporation tube;
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:单圈涡流燃烧器温升稍高的实验研究
机译:被捕获的涡流燃烧器:航空航天和燃气轮机应用的先进燃烧技术
机译:涡流流化床燃烧器(VFBC)干舷中气体/固体流和燃烧的数学建模和实验研究。
机译:通过工业燃气轮机燃烧室的熵扰动的扩散
机译:燃烧引起的涡流击穿对合成气燃气轮机燃烧室闪回限制的影响
机译:三通道扩散器捕集涡流燃烧器扇形钻机的实验与计算研究