Аннотация:
В двумерной нестационарной постановке сформулирована математическая модель непрерывно вращающейся детонационной волны в натекающем сверхзвуковом потоке в кольцевой камере сгорания. Исследована динамика волны в камере в случае газовой водородокислородной смеси. Впервые численно показана возможность реализации при сверхзвуковой скорости потока на входе в диффузор непрерывной спиновой детонации, исследована структура поперечных детонационных волн и область их существования в зависимости от числа Маха потока.
Образец цитирования:
С. А. Ждан, “Математическое моделирование непрерывной спиновой детонации в кольцевой камере сгорания при сверхзвуковой скорости потока”, Физика горения и взрыва, 44:6 (2008), 83–91; Combustion, Explosion and Shock Waves, 44:6 (2008), 690–697
\RBibitem{Zhd08}
\by С.~А.~Ждан
\paper Математическое моделирование непрерывной спиновой детонации в кольцевой камере сгорания при сверхзвуковой скорости потока
\jour Физика горения и взрыва
\yr 2008
\vol 44
\issue 6
\pages 83--91
\mathnet{http://mi.mathnet.ru/fgv1449}
\elib{https://elibrary.ru/item.asp?id=11846396}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2008
\vol 44
\issue 6
\pages 690--697
\crossref{https://doi.org/10.1007/s10573-008-0104-z}
Образцы ссылок на эту страницу:
https://www.mathnet.ru/rus/fgv1449
https://www.mathnet.ru/rus/fgv/v44/i6/p83
Эта публикация цитируется в следующих 37 статьяx:
S. She-Ming Lau-Chapdelaine, Matei I. Radulescu, Zekai Hong, “Quasi-Two-Dimensional Simulation of a Rotating Detonation Engine Combustor and Injector”, Journal of Propulsion and Power, 40:1 (2024), 42
Zhongqi Luo, Hexia Huang, Huijun Tan, Gang Liang, Jinghao Lv, Yuwen Wu, Liugang Li, “On the Self-Similarity in an Annular Isolator under Rotating Feedback Pressure Perturbations”, Aerospace, 10:2 (2023), 188
W K Feng, Q Zheng, Q Xiao, C S Weng, “Numerical study on the propagation characteristics of rotating detonation waves in a ramjet engine”, J. Phys.: Conf. Ser., 2460:1 (2023), 012055
Xixuan Huang, Zhiyong Lin, Yu Liu, Qianmin Wu, “Numerical simulation on the operating characteristics of rotating detonation ramjet engines at high flight mach number”, International Journal of Hydrogen Energy, 48:24 (2023), 9109
Guangyu Wang, Shijie Liu, Haoyang Peng, Weidong Liu, “Experimental Investigation of a Cylindrical Air-Breathing Continuous Rotating Detonation Engine with Different Nozzle Throat Diameters”, Aerospace, 9:5 (2022), 267
V.S. Ivanov, S.M. Frolov, A.E. Zangiev, V.I. Zvegintsev, I.O. Shamshin, “Updated conceptual design of hydrogen/ethylene fueled detonation ramjet: Test fires at Mach 1.5, 2.0, and 2.5”, Aerospace Science and Technology, 126 (2022), 107602
Wei-jie Fan, Jin Zhou, Shi-jie Liu, Hao-yang Peng, “Effects of the geometrical parameters of the injection nozzle on ethylene-air continuous rotating detonation”, J. Zhejiang Univ. Sci. A, 22:7 (2021), 547
Kevin Wu, Shu-jie Zhang, Da-wen She, Jian-ping Wang, “Analysis of flow-field characteristics and pressure gain in air-breathing rotating detonation combustor”, Physics of Fluids, 33:12 (2021)
Kim JuHoe, Takeshi Tsuchiya, AIAA Scitech 2021 Forum, 2021
Weijie Fan, Shijie Liu, Jin Zhou, Haoyang Peng, Siyuan Huang, “Effects of Annular Combustor Width on the Ethylene-Air Continuous Rotating Detonation”, International Journal of Aerospace Engineering, 2020 (2020), 1
Kevin Wu, Shujie Zhang, Mingyi Luan, Jianping Wang, “Effects of flow-field structures on the stability of rotating detonation ramjet engine”, Acta Astronautica, 168 (2020), 174
Qing Xu, Haowei Li, Yaoxun Feng, Xiaoning Li, Changming Ling, Chaoying Zhou, Jiang Qin, “Dynamic thermo-physical characteristics of high temperature gaseous hydrocarbon fuel thermal power generation for regeneratively cooled hypersonic propulsion system”, Energy, 211 (2020), 118722
Jian Sun, Jin Zhou, Shijie Liu, Zhiyong Lin, Wei Lin, “Effects of air injection throat width on a non-premixed rotating detonation engine”, Acta Astronautica, 159 (2019), 189
Jian Sun, Jin Zhou, Shijie Liu, Zhiyong Lin, Wei Lin, “Numerical investigation of a non-premixed hollow rotating detonation engine”, International Journal of Hydrogen Energy, 44:31 (2019), 17084
Vijay Anand, Ephraim Gutmark, “Rotating detonation combustors and their similarities to rocket instabilities”, Progress in Energy and Combustion Science, 73 (2019), 182
S. Hansmetzger, R. Zitoun, P. Vidal, “A study of continuous rotation modes of detonation in an annular chamber with constant or increasing section”, Shock Waves, 28:5 (2018), 1065
Robert Fievisohn, John L. Hoke, Frederick R. Schauer, 2018 AIAA Aerospace Sciences Meeting, 2018
Mohammed Niyasdeen Nejaamtheen, Jung-Min Kim, Jeong-Yeol Choi, Shock Wave and High Pressure Phenomena, Detonation Control for Propulsion, 2018, 109
Andrew R. Mizener, Frank K. Lu, Patrick E. Rodi, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
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