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Effect of wavy wall strut fuel injector on shock wave development and mixing enhancement of fuel and air for a scramjet combustor

机译：波浪墙支柱燃料喷射器对汽轮燃烧室冲击波开发和混合增强的影响

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Obula Reddy Kummitha; K M Pandey;
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1. Numerical investigation of wavy wall strut fuel injector for hydrogen fueled scramjet combustor [J] . Kummitha Obula Reddy, Pandey K. M., Gupta Rajat International journal of hydrogen energy . 2019,第60期

机译：氢燃料超燃燃烧器的波浪式壁撑式喷油器的数值研究
2. Effect of a revolved wedge strut induced mixing enhancement for a hydrogen fueled scramjet combustor [J] . Kummitha Obula Reddy, Pandey K. M., Padidam Anil Kumar Reddy International journal of hydrogen energy . 2021,第24期

机译：旋转楔形支柱诱导混合增强对氢气燃料炒燃烧器的影响
3. Flame Interaction Characteristics in Scramjet Combustor Equipped with Strut/Wall Combined Fuel Injectors [J] . Zhang Junlong, Chang Juntao, Tian Huimin, Combustion Science and Technology . 2020,第10a12期

机译：跳闸燃烧器中的火焰相互作用特性配备支柱/墙壁组合燃料喷射器
4. NUMERICAL SIMULATION OF A HYDROGEN FUELED SCRAMJET COMBUSTOR AT MACH 1.5 USING STRUT INJECTORS AT MACH 2.47 AIR SPEED [C] . K.M.PANDEY, BINITA NATH ASME international mechanical engineering congress and exposition . 2014

机译：在MACH 2.47空气速度下使用支气管喷射器对MACH 1.5处的氢燃料涡扇燃烧器进行数值模拟
5. Hypersonic fuel/air mixing enhancement by cantilevered ramp injectors in the presence of wavy walls. [D] . Alexander, Derrick Clayton. 2001

机译：在波浪形壁的情况下，通过悬臂式坡道喷油器增强高超音速燃料/空气混合。
6. Emission Reduction of Fuel-Staged Aircraft Engine Combustor Using an Additional Premixed Fuel Nozzle [O] . Takeshi Yamamoto, Kazuo Shimodaira, Seiji Yoshida, -1

机译：使用附加的预混合燃料喷嘴减少阶段式飞机发动机燃烧室的排放
7. Investigation of strut-ramp injector in a Scramjet combustor: Effect of strut geometry, fuel and jet diameter on mixing characteristics [O] . Rahul Kumar Soni, Ashoke De 2017

机译：Scramjet燃烧器中支柱坡道注射器的研究：支柱几何，燃料和喷射直径对混合特性的影响
8. Numerical Investigation of Fuel Mixing, Ignition and Flame Stabilization by A Strut Injector in A Scramjet Combustor [R] . Lyubar, A. , Sattelmayer, T. 2002

机译：超燃冲压发动机燃气混合，点火和火焰稳定的数值研究

Effect of wavy wall strut fuel injector on shock wave development and mixing enhancement of fuel and air for a scramjet combustor

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