Rotating Detonation Combustor Downstream Transition Passage Design Considerations
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-90727-3_11
Reference28 articles.
1. Roy, A., Bedick, C.R., Ferguson, D.H., Sidwell, T., Strakey, P.A.: Investigating instabilities in a rotating detonation combustor operating with natural gas–hydrogen fuel blend—effect of air preheat and annulus width. J. Eng. Gas Turbines Power 141(11) (2019)
2. Braun, J., Saracoglu, B.H., Paniagua, G.: Unsteady performance of rotating detonation engines with different exhaust nozzles. J. Propuls. Power 33(1), 121–130 (2017)
3. Anand, V., Gutmark, E.: Rotating detonation combustors and their similarities to rocket instabilities. Prog. Energy Combust. Sci. 73, 182–234 (2019)
4. John, Z.M., et al.: Recent progress, development trends, and consideration of continuous detonation engines. AIAA J. 1–59 (2020)
5. Schwer, D., Kailasanath, K.: Numerical investigation of the physics of rotating-detonation-engines. Proc. Combust. Inst. 33(2), 2195–2202 (2011)
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