CONTROL OF THE SUPERSONIC FLOW STRUCTURE DURING ETHYLENE COMBUSTION WITH THE USE OF GAS-DYNAMIC PULSES

Author:

Zamuraev V. P.,Kalinina A. P.

Publisher

Pleiades Publishing Ltd

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference22 articles.

1. P. K. Tretyakov, V. A. Zabaykin, and A. N. Prokhorov, “High-Velocity Ramjet with a Pulsed Starting Regime," inProc. 11th All-Russian Forum on Fundamental Problems of Mechanics, Kazan’, August 20–24, 2015 (Izd. Kazan. Univ., Kazan’, 2015), pp. 3778–3780.

2. P. K. Tretyakov, V. L. Krainev, A. M. Lazarev, and A. V Postnov,. “Peculiarities of Organization of Effective Hydrocarbon Fuel Combustion in Supersonic Flow," AIP Conf. Proc.2027, 030029 (2018); DOI: 10.1063/1.5065123.

3. S. M. Frolov, V. I. Zvegintsev, V. S. Ivanov, et al., “Demonstrator of a Continuous-Detonation Ramjet. Results of Wind Tunnel Tests," Dokl. Akad. Nauk 474 (1), 51–55 (2017).

4. A. Firsov, K. V. Savelkin, D. A. Yarantsev, and S. B. Leonov, “Plasma-Enhanced Mixing and Flame Holding in Supersonic Flow," Philos. Trans.: Math., Phys. Eng. Sci., Ser. A 373(2048), 20140337 (2015).

5. N. N. Smirnova, V. F. Nikitina, L. I. Stamova, et al., “Three-Dimensional Modeling of Rotating Detonation in a Ramjet Engine," Acta Astronaut. 163, 168–176 (2019); DOI: 10.1016/j.actaastro.2019.02.016.

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