Response of angled and tapered liquid injectors to passing detonation fronts at high operating pressures
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-021-01010-0.pdf
Reference23 articles.
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2. Kailasanath, K.: Review of propulsion applications of detonation waves. AIAA J. 38(9), 1698–1708 (2000). https://doi.org/10.2514/2.1156
3. Lu, F.K., Braun, E.M.: Rotating detonation wave propulsion: experimental challenges, modeling, and engine concepts. J. Propuls. Power 30(5), 1125–1142 (2014). https://doi.org/10.2514/1.B34802
4. Wang, Y.H., Le, J.: How multiple rotating detonation waves are produced. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, AIAA Paper 2018-5202 (2018). https://doi.org/10.2514/6.2018-5202
5. Anand, V., St. George, A., Driscoll, R., Gutmark, E.: Analysis of air inlet and fuel plenum behavior in a rotating detonation combustor. Exp. Ther. Fluid Sci. 70, 408–416 (2016). https://doi.org/10.1016/j.expthermflusci.2015.10.007
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