Effects of ozone addition and LTC progression on detonation of O$$_{3}$$-enhanced DME–O$$_{2}$$
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/s00193-022-01113-2.pdf
Reference71 articles.
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3. Kailasanath, K.: Review of propulsion applications of detonation waves. AIAA J. 38, 1698–1708 (2000). https://doi.org/10.2514/2.1156
4. 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
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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