TY - JOUR
T1 - Development of high-frequency pulse detonation combustor without purging material
AU - Matsuoka, Ken
AU - Muto, Kohei
AU - Kasahara, Jiro
AU - Watanabe, Hiroaki
AU - Matsuo, Akiko
AU - Endo, Takuma
N1 - Publisher Copyright:
Copyright © 2016 by Nagoya University. Published by the American Institute of Aeronautics and Astronautics, Inc.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2017
Y1 - 2017
N2 - A novel method for the operation of a pulse detonation combustor is proposed and demonstrated for realizing high frequencies without using a purging material. In the developed operation method, oxygen is supplied to the pulse detonation combustor in the valveless mode. Fuel, which is supercritical ethylene, is injected into the pulse detonation combustor at a suitable timing using an automotive fuel injector. Because of the Joule-Thomson effect, a phase transition of ethylene from the supercritical state to a low-temperature vapor occurs, and a detonable mixture is produced by mixing with oxygen. In demonstration experiments, a small pulse detonation combustor having an inner diameter of 10 mm, a total length of 190 mm, and an inner volume of 14.5 mL is used, and the operation frequency varies between 100 and 500 Hz. The measured flame propagation speeds are 107 ± 6% of the Chapman-Jouguet detonation speed. In addition, the operation frequency of 500 Hz is 41% of the gas-dynamic upper limit, which is obtained using the one-dimensional model proposed by Endo et al.
AB - A novel method for the operation of a pulse detonation combustor is proposed and demonstrated for realizing high frequencies without using a purging material. In the developed operation method, oxygen is supplied to the pulse detonation combustor in the valveless mode. Fuel, which is supercritical ethylene, is injected into the pulse detonation combustor at a suitable timing using an automotive fuel injector. Because of the Joule-Thomson effect, a phase transition of ethylene from the supercritical state to a low-temperature vapor occurs, and a detonable mixture is produced by mixing with oxygen. In demonstration experiments, a small pulse detonation combustor having an inner diameter of 10 mm, a total length of 190 mm, and an inner volume of 14.5 mL is used, and the operation frequency varies between 100 and 500 Hz. The measured flame propagation speeds are 107 ± 6% of the Chapman-Jouguet detonation speed. In addition, the operation frequency of 500 Hz is 41% of the gas-dynamic upper limit, which is obtained using the one-dimensional model proposed by Endo et al.
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U2 - 10.2514/1.B36068
DO - 10.2514/1.B36068
M3 - Article
AN - SCOPUS:85012231864
SN - 0748-4658
VL - 33
SP - 43
EP - 50
JO - Journal of Propulsion and Power
JF - Journal of Propulsion and Power
IS - 1
ER -