Fizika Goreniya i Vzryva, 2009, Volume 45, Issue 6, Pages 91–104(Mi fgv1355)
This article is cited in 14 scientific papers (total in 14 papers)
Realization and modeling of continuous spin detonation of a hydrogen-oxygen mixture in flow-type combustors. 2. Combustors with expansion of the annular channel
Abstract:
Results of a comprehensive numerical and experimental study of continuous spin detonation of an H2–O2 mixture in flow-type annular combustors with channel expansion are presented. In these experiments, oxygen is supplied as a continuous flow through an annular slot, and hydrogen is injected through injectors. Combustion of hydrogen-oxygen mixtures in continuously rotating (spinning) and pulsed detonation waves with exhaustion of the products into an evacuated tank with increasing counterpressure and into the atmosphere was realized and studied in such combustors for the first time. The domain of realization of continuous detonation is determined. Verification of the mathematical model is performed on the basis of experimental results, and reasonable agreement is reached for the basic detonation parameters: structure of transverse detonation waves, their velocity, and pressures in the combustor and in the injection system.
Citation:
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Realization and modeling of continuous spin detonation of a hydrogen-oxygen mixture in flow-type combustors. 2. Combustors with expansion of the annular channel”, Fizika Goreniya i Vzryva, 45:6 (2009), 91–104; Combustion, Explosion and Shock Waves, 45:6 (2009), 716–728
This publication is cited in the following 14 articles:
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Guangyao Rong, Miao Cheng, Yunzhen Zhang, Zhaohua Sheng, Jianping Wang, “Investigation of flow field characteristics and performance of carbon–hydrogen/oxygen-rich air rotating detonation engine”, Physics of Fluids, 35:9 (2023)
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Zhenjuan Xia, Hu Ma, Changfei Zhuo, Changsheng Zhou, “Propagation characteristics of rotating detonation wave in plane–radial structure with different pressure conditions”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233:7 (2019), 2378
Qiaofeng Xie, Bing Wang, Haocheng Wen, Wei He, “Thermoacoustic Instabilities in an Annular Rotating Detonation Combustor Under Off-Design Condition”, Journal of Propulsion and Power, 35:1 (2019), 141
Zhenhua Pan, Kaipeng Chen, Jun Qi, Penggang Zhang, Yuejin Zhu, Jianfeng Pan, Mingyue Gui, “The propagation characteristics of curved detonation wave: Experiments in helical channels”, Proceedings of the Combustion Institute, 37:3 (2019), 3585
Zhenhua Pan, Jun Qi, Jianfeng Pan, Penggang Zhang, Yuejin Zhu, Mingyue Gui, “Fabrication of a helical detonation channel: Effect of initial pressure on the detonation propagation modes of ethylene/oxygen mixtures”, Combustion and Flame, 192 (2018), 1
XuDong Zhang, BaoChun Fan, MingYue Gui, ZhenHua Pan, “Cellular structure of detonation utilized in propulsion system”, Sci. China Phys. Mech. Astron., 55:10 (2012), 1915
Zhenhua Pan, Baochun Fan, Xudong Zhang, Mingyue Gui, Gang Dong, “Wavelet pattern and self-sustained mechanism of gaseous detonation rotating in a coaxial cylinder”, Combustion and Flame, 158:11 (2011), 2220
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 2. Air as an oxidizer”, Combustion, Explosion and Shock Waves, 47:2 (2011), 217–225
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 1. Oxygen as a oxidizer”, Combustion, Explosion and Shock Waves, 46:3 (2010), 344–351
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