@article{oai:nagoya.repo.nii.ac.jp:00027944,
 author = {Yamaguchi, Masato and Matsuoka, Ken and Kawasaki, Akira and Kasahara, Jiro and Watanabe, Hiroaki and Matsuo, Akiko},
 issue = {3},
 journal = {Proceedings of the Combustion Institute},
 month = {},
 note = {As a novel detonation combustor that differs from a pulse and a rotating detonation engine, a reflective shuttling detonation combustor (RSDC), in which detonation waves shuttle repeatedly, was proposed. In a fan-shaped two-dimensional combustor, detonation waves propagate, repeating attenuation and re-ignition by a shock reflection at the side wall. In the demonstration experiment, chemiluminescence visualization and pressure measurement with ethylene–oxygen mixture were conducted at the same time. As the result, a single shuttling wave coupled with pressure rise was observed in the combustor. The tangential velocity of the wave was 1526 ± 12 m/s and approximately 60% of the estimated Chapman–Jouguet velocity of 2513 m/s. The ratio of pressure in front of the wave to one behind the primary wave or the reflected wave was in good agreement with one-dimensional shock theory, and it was suggested that the rapid reaction behind the reflected shock wave sustained the continuous propagation of the shock wave., ファイル公開：2021-01-01},
 pages = {3741--3747},
 title = {Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor},
 volume = {37},
 year = {2019}
}