Dependence of premixture jet height on detonation wave propagation inside a pressure gain combustion channel

Author:

Wang Faming1,Kitaori Taichi1,Shimizu Ryunosuke1,Mizukaki Toshiharu1

Affiliation:

1. Tokai Daigaku

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. Toshiharu, M., Fumihiko, I., Makoto, K., Hideto, K., Shingo, M., Kazuya, I., Yoshio, N., Hideyuki,T. "Flow Visualization inside a Rotating Detonation Engine near Injection Nozzles Using Point-Diffraction Interferometry," AIAA 2021-0417. DOI: 10.2514/6.2021-041710.2514/6.2021-0417

2. Shingo, M., Kazuya, I., Yoshio, N., Hideyuki, T., Toshiharu, M., Makoto, K., and Hideto, K. "Large-Eddy Simulation of Rotating Detonation with a Non-premixed CH4/O2Injection," AIAA 2020-1174. DOI: 10.2514/6.2020-117410.2514/6.2020-1174

3. Yungster, S., Radhakrishnan, K., and Perkins, H,D. "Structure and Stability of One-Dimensional Detonations in Ethylene-Air Mixtures," AIAA Paper 2003-4248, E-14143. DOI: 10.2514/6.2003-424810.2514/6.2003-4248

4. Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine

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