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机译:不同腔长度与深度比例的单面膨胀瘙痒型燃烧器中火焰稳定的实验研究
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;
Injection scheme; Length-to-depth ratio; Combustion stabilization mode; Flame oscillations;
机译:具有后壁扩展腔的超燃冲压燃烧器的火焰稳定实验
机译:具有后壁膨胀腔的超燃冲压燃烧器火焰稳定过程的大涡模拟
机译:腔参数对单侧膨胀超燃燃烧室燃烧振荡的影响
机译:圆锥撑杆和型腔火焰架的圆形超燃燃烧室煤油点火实验研究
机译:在稀薄预混燃气轮机燃烧室中技术预混火焰中强制火焰响应的实验研究。
机译:带有小火箭排气的Strutjet RBCC燃烧器的点火和火焰稳定
机译:空气节流对乙烯燃料炒燃烧器火焰稳定的影响研究
机译:使用kHz帧率OH-pLIF和stereo-pIV的燃气轮机模型燃烧室中涡流稳定Lpp火焰自燃现象的实验研究