Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers

机译：高超声速马赫数下的烃类燃料超燃冲压发动机研究

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Planar laser-induced fluorescence (PLIF) of OH and wall-pressure measurements have been used to investigate the combustion in a cavity flame- holder scramjet combuster.

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Houwing, F.;
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年度 2005
页码 1-138
总页数 138
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Hydrocarbons; Mach number; Supersonic combustion ramjet engines; Laser induced fluorescence; Combustion; Flame holders; Hypersonic velocity; Australia; Planar structures; Fuels;

机译：碳氢化合物;马赫数;超音速燃烧冲压式喷气发动机;激光诱导荧光;燃烧;火焰稳定器;高超声速;澳大利亚;平面结构;燃料;

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专利

1. Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement [J] . Aerospace science and technology . 2020,第Mara期

机译：巡航约束和燃烧室冷却要求下碳氢燃料超燃发动机的最大飞行马赫数分析
2. Mach 6-8+ Hydrocarbon-Fueled Scramjet Flight Experiment: The HIFiRE Flight 2 Project [J] . Kevin R. Jackson, Mark R. Gruber, Salvatore Buccellato Journal of propulsion and power . 2015,第1期

机译：6-8马赫以上的碳氢燃料超燃冲压发动机飞行实验：HIFiRE 2飞行项目
3. Investigation of local unstart in a hypersonic scramjet intake at a Mach number of 6 [J] . Devaraj Manoj Kumar K., Jutur Prahallada, Rao Srisha M. V, Aerospace science and technology . 2021,第Auga期

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4. Design of Hypersonic Scramjet Engine Operating between Mach 5 to Mach 9 [C] . Daniyal Ahmed Khan, M. Hammad Hassan, Ihtzaz Qamar International Conference on Aerospace Science and Engineering . 2019

机译：在5马赫至9马赫之间运行的超音速超燃冲压发动机的设计
5. Analysis and design of a hypersonic scramjet engine with a starting Mach number of 4.00 [D] . Roberts, Kristen Nicole 2008

机译：马赫数为4.00的高超音速超燃冲压发动机的分析和设计
6. Saccharibacteria as Organic Carbon Sinks in Hydrocarbon-Fueled Communities [O] . Perla Abigail Figueroa-Gonzalez, Till L. V. Bornemann, Panagiotis S. Adam, 2020

机译：糖酸酯作为碳氢化合物燃料社区的有机碳汇
7. Radical recombination in a hydrocarbon-fueled scramjet nozzle [O] . Zhang Xiaoyuan, Qin Lizi, Chen Hong, 2014

机译：碳氢燃料超燃冲压发动机喷嘴中的自由基重组

Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers

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