Effects of the geometrical parameters of the injection nozzle on ethylene-air continuous rotating detonation
Author:
Funder
National Natural Science Foundation of China
the Postgraduate Scientific Research Innovation Project of Hunan Province, China
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2000314.pdf
Reference55 articles.
1. Anand V, George ACS, Driscoll RB, et al., 2015. Statistical treatment of wave instability in rotating detonation combustors. Proceedings of the 53rd AIAA Aerospace Sciences Meeting. https://doi.org/10.2514/6.2015-1103
2. Anand V, George AS, Driscoll R, et al., 2016a. Analysis of air inlet and fuel plenum behavior in a rotating detonation combustor. Experimental Thermal and Fluid Science, 70:408–416. https://doi.org/10.1016/j.expthermflusci.2015.10.007
3. Anand V, George AS, Driscoll R, et al., 2016b. Investigation of rotating detonation combustor operation with H2-air mixtures. International Journal of Hydrogen Energy, 41(2):1281–1292. https://doi.org/10.1016/j.ijhydene.2015.11.041
4. Bykovskii FA, Vedernikov EF, 1996. Self-sustaining pulsating detonation of gas-mixture flow. Combustion, Explosion and Shock Waves, 32(4):442–448. https://doi.org/10.1007/BF01998496
5. Cai XD, Liang JH, Deiterding R, et al., 2016. Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model. International Journal of Hydrogen Energy, 41(4):3222–3239. https://doi.org/10.1016/j.ijhydene.2015.11.093
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Numerical study on ethylene-air continuous rotating detonation in annular combustors with different widths;Journal of Zhejiang University-SCIENCE A;2022-05
2. Erratum to: Effects of the geometrical parameters of the injection nozzle on ethylene-air continuous rotating detonation;Journal of Zhejiang University-SCIENCE A;2022-02
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