Effects of thermal pretreatment and equivalence ratio on DME/$${\hbox {O}}_2$$/$${\hbox {O}}_3$$ detonations
Author:
Funder
National Aeronautics and Space Administration
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-023-01147-0.pdf
Reference73 articles.
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3. Zhou, R., Wu, D., Wang, J.: Progress of continuously rotating detonation engines. Chin. J. Aeronaut. 29, 15–29 (2016). https://doi.org/10.1016/j.cja.2015.12.006
4. Luan, Z., Huang, Y., Gao, S., You, Y.: Formation of multiple detonation waves in rotating detonation engines with inhomogeneous methane/oxygen mixtures under different equivalence ratios. Combust. Flame 241, 112091 (2022). https://doi.org/10.1016/j.combustflame.2022.112091
5. Wolański, P.: Detonative propulsion. Proc. Combust. Inst. 34, 125–158 (2013). https://doi.org/10.1016/j.proci.2012.10.005
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