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Numerical study on ethylene-air continuous rotating detonation in annular combustors with different widths

Journal of Zhejiang University-Science A(Applied Physics & Engineering) 2022年第5期23卷 388-404页

作者： Wei-jie FAN Wei-dong LIU Hao-yang PENG Shi-jie LIU Jian SUN Science and Technology on Scramjet Laboratory College of Aerospace Science and TechnologyNational University of Defense TechnologyChangsha 410073China State Key Laboratory of Aerospace Dynamic Satellite Control CenterXi’an 710043China

To investigate the impact of combustor width on continuous rotating detonation(CRD)fueled by ethylene and air,a series of 3 D simulations are conducted by changing the inner cylinder radius of an annular combustor while retaining the same outer cylinder radius.The results show that the CRD wave propagates more steadily and faster as the combustor width increases.The high-temperature zone at the backward-facing step preheats the propellants and contributes to the steady propagation of the CRD wave in 25-and 30-mm wide combustors.The highest and the lowest velocities are obtained in the30-and 15-mm wide combustors at,respectively,1880.27 and 1681.01 m/s.On the other hand,the average thrust decreases as the combustor width increases.The highest thrust is obtained in the 15-mm wide combustor while the lowest is in the 30-mm wide combustor,at 758.06 and 525.93 N,respectively.Nevertheless,the thrust is much more stable in the 25-and 30-mm wide combustors than in the 15-and 20-mm wide combustors.

关键词： Continuous rotating detonation(CRD) Ethylene-air Combustor width propagation mode Propulsive performance

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Experimental study on propagation characteristics of rotating detonation wave with kerosene fuel-rich gas

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Defence Technology（防务技术） 2022年第8期18卷 1498-1512页

作者： Jia-xiang Han Qiao-dong Bai Shi-jian Zhang Fang Wang Chun-sheng Weng National Key Laboratory of Transient Physics Nanjing University of Science and TechnologyNanjing210094China

In this study, kerosene fuel-rich gas produced by the combustion in the gas generator was used as the fuel and oxygen-rich air was used as the oxidant to investigate the propagation characteristics of the rotating detonation wave (RDW). The initiation of the kerosene fuel-rich gas and propagation process of the RDW were analyzed. The influences of the oxygen content in the oxidizer, kerosene mass flow rate of the gas generator, and temperature of the kerosene fuel-rich gas on the propagation process of the RDW were studied. The experimental results revealed that the propagation velocity of the RDW could be improved by increasing the three parameters mentioned above with the kerosene mass flow rate as the strongest factor. The minimum oxygen content that could successfully initiate and maintain the stable propagation of the RDW was 32%, achieving the RDW velocity of 1141.9 m/s. The RDW mainly propagated as two-counter rotating waves and a single wave when the equivalent ratios were 0.62–0.79 and 0.85–0.87, respectively. The highest RDW velocity of 1637.2 m/s was obtained when the kerosene mass flow rate, oxygen content, and equivalent ratio were 74.6 g/s, 44%, and 0.87, respectively.

关键词： Rotating detonation wave Kerosene fuel-rich gas Initiation process propagation mode

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