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Cavity- Based Injector Mixing Experiments for Supersonic Combustors with Implications on Igniter Placement

机译：基于腔的喷射器混合实验，用于超音速燃烧器，对点火器放置的影响

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《American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/Society of Automotive Engineers/American Society for Engineering Education Joint Propulsion Conference Exhibit》|2006年||共13页
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1. Distribution characteristics and mixing mechanism of a liquid jet injected into a cavity-based supersonic combustor [J] . Li Peibo, Li Chenyang, Wang Hongbo, Aerospace science and technology . 2019,第Nova期

机译：腔内超音速燃烧室中喷射液体的分布特性及混合机理
2. Influence of combustor inlet conditions on combustor exit gas peak temperature factor (experiment by using the combustor with pressure atomizing fuel nozzles and the combustor with airblast type fuel injectors) [J] . Sato Yukinori, Toh Hidemi, Watanabe Takeshi, Bulletin of GTSJ . 2002,第2002期

机译：燃烧室入口条件对燃烧室出口气体峰值温度因子的影响（通过使用带有压力雾化燃料喷嘴的燃烧室和带有鼓风型燃料喷射器的燃烧室进行的实验）
3. Influence of combustor inlet condition on combustor exit gas peak temperature factor (experiment by using the combustor with pressure atomizing fuel nozzles and the combustor with airblast type fuel injectors) [J] . Sato Yukinori, Toh Hidemi, Watanabe Takeshi, 日本ガスタ-ビン学会誌 . 2001,第1期

机译：燃烧室入口条件对燃烧室出口气体峰值温度系数的影响（通过使用带有压力雾化燃料喷嘴的燃烧室和带有鼓风型燃料喷射器的燃烧室进行的实验）
4. Cavity- Based Injector Mixing Experiments for Supersonic Combustors with Implications on Igniter Placement [C] . L. Jacobsen, C. Carter, A. Dwenger AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2006

机译：基于腔的喷油器混合实验对超音速燃烧器的点火器位置影响
5. An integrated aerodynamic-ramp-injector/plasma-torch-igniter for supersonic combustion applications with hydrocarbon fuels. [D] . Jacobsen, Lance Steven. 2001

机译：集成的气动坡道喷油器/等离子炬点火器，用于碳氢燃料的超音速燃烧应用。
6. 3D15N/15N/1H Chemical Shift Correlation Experiment Utilizing an RFDR-based 1H/1H Mixing Period at 100 kHz MAS [O] . Yusuke Nishiyama, Michal Malon, Yuji Ishii, -1

机译：3D15N / 15N / 1H化学位移相关实验使用基于RFDR的1H / 1H混合周期（100 kHz MAS）
7. A numerical study of mixing in supersonic combustors with hypermixing injectors [O] . J. LEE 1993

机译：用超声喷射器混合在超声燃烧器中混合的数值研究
8. Cavity-Based Injector Mixing Experiments for Supersonic Combustors With Implications on Igniter Placement (Postprint) [R] . Jacobsen, L. S. , Carter, C. D. , Dwenger, A. C. 2006

机译：基于腔体的超音速燃烧器喷射器混合实验及对点火器放置的影响（后印刷）

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