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Injection and Mixing of Gas Propellants for Pulse Detonation Propulsion

机译：用于脉冲爆轰推进的气体推进剂的注入和混合

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Dora Elia Musielak;
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年度 2015
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1. Experimental Study of Propulsion Performance by Single-Pulse Rotating Detonation with Gaseous Fuels-Oxygen Mixtures [J] . Toshimitsu Kazuhiko, Hara Kosei, Mikajiri Shuuto, International Journal of Turbo and Jet Engines . 2016,第4期

机译：气态燃料-氧气混合气单脉冲旋转爆轰推进性能的实验研究
2. Investigation into the transient flow characteristics of noble gas propellants using the pulsed inductive discharge in electric propulsion [J] . Yuguo CHENG, Guangqing XIA 中国航空学报（英文版） . 2020,第009期

机译：用电推进中的脉冲感应放电研究稀有气体推进剂的瞬态流动特性
3. Study on operation and propulsion features of a pulse detonation rocket engine with secondary oxidizer injection [J] . Zhang Qibin, Qiao Xinqi, Fan Wei, Applied thermal engineering: Design, processes, equipment, economics . 2020,第1期

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4. Propulsion from the Pulse Detonation of Solid Propellant Pellet- Projectiles [C] . V. Krishnan AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2006

机译：固体推进剂药丸的脉冲爆轰产生的推进力
5. Transient analysis of a pulsed detonation combustor using the numerical propulsion system simulation. [D] . Hasler, Anthony Scott. 2012

机译：使用数值推进系统仿真对脉冲爆震燃烧室进行瞬态分析。
6. Design of a Novel Axial Gas Pulses Micromixer and Simulations of its Mixing Abilities via Computational Fluid Dynamics [O] . Florian Noël, Christophe A. Serra, Stéphane Le Calvé 2016

机译：新型轴向气体脉冲微混合器的设计及其混合能力的计算流体动力学模拟
7. Deuterium-Tritium Pulse Propulsion with Hydrogen as Propellant and the Entire Spacecraft as a Gigavolt Capacitor for Ignition [O] . Winterberg, Friedwardt 2012

机译：氘 - 氚脉冲推进氢气作为推进剂和整个航天器作为Gigavolt点火器的电容器

Injection and Mixing of Gas Propellants for Pulse Detonation Propulsion

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