Faculty Profiles - MATSUOKA Ken

Papers - MATSUOKA Ken

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Experimental Demonstration on Detonation Initiation by Laser Ignition and Shock Focusing in Elliptical Cavity Reviewed

T. Sato, K. Matsuoka, A. Kawasaki, N. Itouyama, H. Watanabe, J. Kasahara

Shock Waves Vol. 33 page： 521 - 531 2024.1

Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space Reviewed

V. Buyakofu, K. Matsuoka, K. Matsuyama, K. Kawasaki, H. Watanabe, N. Itouyama, K. Goto, K. Ishihara, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada

Journal of Spacecraft and Rockets Vol. 60 ( 1 ) page： 181 - 189 2023.9

Lagrangian dispersion and averaging behind a two-dimensional gaseous detonation front Reviewed International coauthorship

H. Watanabe, A. Matsuo, A. Chinnayya, N. Itouyama, A. Kawasaki, K. Matsuoka, J. Kasahara

Journal of Fluid Mechanics Vol. 968 ( A28 ) 2023.8

Impact of mixture mass flux on hydrodynamic blockage ratio and Mach number of rotating detonation combustor Reviewed

T, Noda, K. Matsuoka, K. Goto, A. Kawasaki, H. Watanabe, N. Itouyama, J. Kasahara, A. Matsuo

Acta Astronautica 2023.3

Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine Reviewed

K. Ishihara, K. Yoneyama, H. Watanabe, N. Itouyama, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, K. Higashino

Journal of Propulsion and Power Vol. 39 ( 3 ) page： 297 - 307 2023.2

Visualization and performance evaluation of liquid-ethanol cylindrical rotating detonation combustor Reviewed

K. Ishihara, K. Yoneyama, T. Sato, H. Watanabe, N. Itouyama, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki

Transactions of JSAS Vol. 66 ( 2 ) page： 46 - 58 2023

Numerical investigation of the effects of injector configuration on flow structures in annular and cylindrical rotating detonation combustors Reviewed

Vol. 84 ( 2 ) page： 17 - 23 2023

Effect of Channel Expansion Angle near Injector Outlet on a Rotating Detonation Engine Performance Reviewed

K. Nakajima, K. Matsuoka, N. Itouyama, J. Kasahara, A. Kawasaki, A. Matsuo,

Shock Waves 2023

Combustion Structure of a Cylindrical Rotating Detonation Engine with Liquid Ethanol and Nitrous Oxide Reviewed

T. Sato, K. Nakata, K. Ishihara, N. Itouyama, K. Matsuoka, J. Kasahara, A. Kawasaki, D. Nakata, H. Eguchi, M. Uchiumi, A. Matsuo, I. Funaki

Combustion and Flame 2023

Assessment of the sensitivity to detonation of the gaseous pyrolytic products formed during the thermal decomposition of ammonium dinitramide and its related ionic liquids Reviewed

N. Itouyama, X. Huang, R. Mével, K. Matsuoka, J. Kasahara, H. Habu

Shock Waves 2023

Experimental Investigation of Innner Flow of a Throatless Diverging Rotating Detonation Engine Reviewed International coauthorship

K. Nakata, K. Ishihara, K. Goto, N. Itouyama, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, K. Higashino, J. Braun, T. Meyer, G. Paniagua

Proceedings of the Combustion Institute Vol. 39 ( 3 ) page： 3073 - 3082 2022.11

Experimental Study on Detonation-Diffraction Reflection Point Distances in Hydrogen and Gaseous Hydrocarbon Reactive Systems Invited Reviewed

H. Sun, A. Kawasaki, N. Itouyama, K. Matsuoka, J. Kasahara

combustion and flame Vol. 245 2022.11

Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-3 Reviewed

K. Goto, K. Matsuoka, K. Matsuyama, K. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada

Journal of Spacecraft and Rockets Vol. 60 ( 1 ) page： 273 - 285 2022.10

Investigation of Reflective Shuttling Detonation Cycle by Schlieren and Chemiluminescence Photography Reviewed

T. Taguchi, K. Matsuoka, M. Yamaguchi, K. Kawasaki, H. Watanabe, N. Itouyama, A. Matsuo, J. Kasahara

Combustion and Flame Vol. 236 2022.2

Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket Reviewed

V. Buyakofu, K. Matsuoka, K. Matsuyama, K. Kawasaki, H. Watanabe, N. Itouyama, K. Goto, K. Ishihara, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M, Uchiumi, H, Habu, Shinsuke Takeuchi, S. Arakawa, J. Masuda, K. Maehara

Journal of Spacecraft and Rockets 2022.1

Supersonic Exhaust from a Rotating Detonation Engine with Throatless Diverging Channel Reviewed

K. Nakata, K. Ota, K. Ishihara, K. Goto, N. Itouyama, H. Watanabe, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, K. Higashino, J. Braun, T. Meyer, G. Paniagua

AIAA journal 2022

Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled Test Reviewed

K. Goto, Y. Kato, K. Ishihara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, K. Higashino, N. Tanatsugu

Journal of Propulsion and Power Vol. 37 ( 3 ) page： 419 - 425 2021.12

Cylindrical Rotating Detonation Engine with Propellant Injection Cooling Invited Reviewed

K. Goto, K. Ota, K. Kawasaki, N. Itouyama, H. Watanabe, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Kawashima

Journal of Propulsion and Power 2021.11

Cylindrical Rotating Detonation Engine with Propellant Injection Cooling Reviewed

2021.11

Torque Around the Axial Direction on Rotating Detonation Engines Invited Reviewed

S. Sawada, K. Goto, K. Ishihara, K. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki

Journal of Propulsion and Power 2021.9

Investigation of the Effect of Triplet Injector Hole on Propulsive Performance of Rotating Detonation Engine Invited Reviewed

K. Goto, R. Yokoo, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Kawashima

Shock Waves 2021.3

Experimental investigation on a rotating detonation cycle with burned gas backflow Reviewed

Matsuoka Ken, Tanaka Masaya, Noda Tomoyuki, Kawasaki Akira, Kasahara Jiro

COMBUSTION AND FLAME Vol. 225 page： 13 - 19 2021.3

Investigation of the Effect of Triplet Injector Hole on Propulsive Performance of Rotating Detonation Engine Invited Reviewed

K. Goto, R. Yokoo, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Kawashima

Shock Waves 2021.1

Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket Invited Reviewed

Journal of Spacecraft and Rockets 2021

Propulsion Performance of Cylindrical Rotating Detonation Engine Reviewed International journal

R. Yokoo, K. Goto, J. Kim, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki

AIAA Journal Vol. 58 ( 12 ) page： 5107 - 5116 2020.12

Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled-Test Invited Reviewed

K. Goto, Y. Kato, K. Ishihara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, K. Higashino, N. Tanatsugu

Journal of Propulsion and Power 2020.11

Numerical analysis on behavior of dilute water droplets in detonation Reviewed

H. Watanabe, A. Matsuo, A. Chinnayya, K. Matsuoka, A. Kawasaki, J. Kasahara

Proceedings of the Combustion Institute 2020.10

A Study on Detonation-Diffraction Reflection Point Distances in H2/O2, C2H2/O2, and C2H4/O2 Systems Reviewed

H. Sun, A. Kawasaki, K. Matsuoka, J. Kasahara

Proceedings of the Combustion Institute page： (Accepted for Publication) 2020.9

Investigation of combustion modes and pressure of reflective shuttling detonation combustor Reviewed

M, Yamaguchi, T. Taguchi, K. Matsuoka, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo

Proceedings of the Combustion Institute page： (Accepted for Publication) 2020.9

Experimental Study of Internal Flow Structures in Cylindrical Rotating Detonation Engines Reviewed

R. Yokoo, K. Goto, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki

Proceedings of the Combustion Institute 2020.8

Numerical analysis of the mean structure of gaseous detonation with dilute water spray

Watanabe Hiroaki, Matsuo Akiko, Chinnayya Ashwin, Matsuoka Ken, Kawasaki Akira, Kasahara Jiro

JOURNAL OF FLUID MECHANICS Vol. 887 2020.3

Investigation of the Measurement Characteristics of a Multiple ion probe Method for a Propagating Methane oxygen nitrogen Flame Reviewed

T. Yatsufusa, K. Kii, N. Miura, H, Yamamoto, A. Kawasaki, K. Matsuoka, J. Kasahara

Combustion and Flame Vol. 211 page： 1-12 2019.10

Semi-Valveless Pulse Detonation Cycle at a Kilohertz-scale Operating Frequency, Reviewed

K. Matsuoka, H. Taki, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo

Combustion and Flame Vol. 205 2019.5

Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles International journal

Goto Keisuke, Nishimura Junpei, Kawasaki Akira, Matsuoka Ken, Kasahara Jiro, Matsuo Akiko, Funaki Ikkoh, Nakata Daisuke, Uchiumi Masaharu, Higashino Kazuyuki

JOURNAL OF PROPULSION AND POWER Vol. 35 ( 1 ) page： 213-223 2019.1

Critical condition of inner cylinder radius for sustaining rotating detonation waves in rotating detonation engine thruster International journal

Kawasaki Akira, Inakawa Tomoya, Kasahara Jiro, Goto Keisuke, Matsuoka Ken, Matsuo Akiko, Funaki Ikkoh

PROCEEDINGS OF THE COMBUSTION INSTITUTE Vol. 37 ( 3 ) page： 3461 - 3469 2019

Numerical investigation on propagation behavior of gaseous detonation in water spray International journal

Watanabe Hiroaki, Matsuo Akiko, Matsuoka Ken, Kawasaki Akira, Kasahara Jiro

PROCEEDINGS OF THE COMBUSTION INSTITUTE Vol. 37 ( 3 ) page： 3617 - 3626 2019

Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor International journal

Yamaguchi Masato, Matsuoka Ken, Kawasaki Akira, Kasahara Jiro, Watanabe Hiroaki, Matsuo Akiko

PROCEEDINGS OF THE COMBUSTION INSTITUTE Vol. 37 ( 3 ) page： 3741-3747 - 3747 2019

Optical Measurement of Fluid Motion in Semi-Valveless Pulse Detonation Combustor with High-Frequency Operation Reviewed

A. Kubota, K. Matsuoka, A. Kawasaki, J. Kasahara, A. Matsuo, H. Watanabe,T. Endo

Combustion Science and Technology 2018.12

Validation of Pulse-Detonation Operation in Low-Ambient-Pressure Environment International journal

Ken Matsuoka, Shunsuke Takagi, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki

JOURNAL OF PROPULSION AND POWER Vol. 34 ( 1 ) page： 116 - 124 2018.1

Language：English Publishing type：Research paper (scientific journal) Publisher：AMER INST AERONAUTICS ASTRONAUTICS

A pulse-detonation thruster can generate a high-repeatability small impulse at a high operating frequency. To operate a pulse-detonation cycle in a vacuum environment without a purging material, a liquid-purge method proposed by Matsuoka et al. ("Development of a Liquid-Purge Method for High-Frequency Operation of Pulse Detonation Combustor," Combustion Science and Technology, Vol. 187, No. 5, 2015, pp. 747-764) and throat at the exit of the combustor were introduced. In the demonstration experiment, gaseous ethylene-liquid nitrous oxide, as detonable mixture, and a throat having an inner diameter of 3.6 mm (blockage ratio = 87%) were used. The measured cyclic flame-propagation speeds were 2005 +/- 90 m/s and 92 +/- 4% of the estimated Chapman-Jouguet detonation speed. Consequently, a 50 Hz pulse-detonation operation without a purging material in the ambient-pressure range of 0.035-1.5 kPa was confirmed. A quasi-steady model, in which gases in the combustor are in the stationary state, was newly developed to investigate the operating characteristic of the pulse-detonation thruster. The experimental pressure history in the combustor during the burned-gas blowdown process was in good agreement with that of the model. Moreover, using the model, the thrust performance of the pulse-detonation thruster with a converging-diverging nozzle was investigated. It was found that the estimated specific impulse was comparable with that of the theoretical steady-state rocket engine.

DOI： 10.2514/1.B36401

Web of Science

Development of High-Frequency Pulse Detonation Combustor without Purging Material Reviewed

K., Matsuoka, K., Muto, J., Kasahara, H., Watanabe, A., Matsuo, and T., Endo

Journal of Propulsion and Power Vol. 33 page： 43-50 2017

Reduction of air flow rate for pulse-detonation-turbine-engine operation by water-droplet injection Reviewed

T. Endo, K. Masuda, W. Watanabe, T. Mukai, H. Nagai, J. Johzaki, K. Matsuoka,

Journal of Thermal Science and Technology 2016.9

Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor

S. Nakagami, K. Matsuoka, J. Kasahara, Y. Kumazawa, J. Fujii, A. Matsuo, and I. Funaki

Journal of Propulsion and Power 2016

Numerical Investigation on Detonation Velocity in Rotating Detonation Engine Chamber Reviewed

J. Fujii, Y. Kumazawa, A. Matsuo, S. Nakagami, K. Matsuoka, J. Kasahara,

Proceedings of the Combustion Institute 2016

Experimental Study of the Structure of Forward-Tilting Rotating Detonation Waves and Highly Maintained Combustion Chamber Pressure in a Two-Parallel-Plane Combustor Reviewed

S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki

Proceedings of the Combustion Institute 2016

Investigation of Fluid Motion in Valveless Pulse Detonation Combustor with High-Frequency Operation Reviewed

K. Matsuoka, K. Muto, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo,

Proceedings of the Combustion Institute 2016

Thermal Spray using a High-Frequency Pulse Detonation Combustor Operated in the Liquid-Purge Mode Reviewed

T., Endo, R., Obayashi, T., Tajiri, K., Kimura, Y., Morohashi, T., Johzaki, K., Matsuoka, T., Hanafusa, S., Mizunari

Journal of Thermal Spray Technology Vol. 25 ( 3 ) page： pp. 494-508 2015

Flight Validation of a Rotary-Valved Four-Cylinder Pulse Detonation Rocket Reviewed

K., Matsuoka, T., Morozumi, S., Takagi, J., Kasahara, A., Matsuo, and I., Funaki

Journal of Propulsion and Power 2015

Thrust Performance of Rotary-Valved Four-Cylinder Pulse Detonation Rocket Engine Reviewed

K., Matsuoka, R., Sakamoto, T., Morozumi, J., Kasahara, A., Matsuo, and I., Funaki

Transactions of the JSASS Vol. 58 ( 4 ) page： pp. 193-203 2015

Development of a Liquid-Purge Method for High-Frequency Operation of Pulse Detonation Combustor Reviewed

K., Matsuoka, T., Mukai, T., Endo

Combustion Science and Technology Vol. 187 ( 5 ) page： pp. 747-764 2015

Optical and Thrust Measurement of a Pulse Detonation Combustor with a Coaxial Rotary Valve Reviewed

K., Matsuoka, M., Esumi, K., Ikeguchi, J., Kasahara, A., Matsuo and I., Funaki

Combustion and Flame Vol. 159 ( 3 ) page： pp. 1321-1338 2012

Experimental Investigation of a Multi-Cycle Single-Tube Pulse Detonation Rocket Engine with a Coaxial Rotary Valve Reviewed

K., Matsuoka, M., Esumi, K., B., Ikeguchi, J., Kasahara, A., Matsuo and I., Funaki

Transaction of JSASS Aerospace Technology Japan Vol. 10 ( 3 ) page： pp. Te_1-4 2012

Inflow-Driven Valve System for Pulse Detonation Engines Reviewed

K., Matsuoka, J., Yageta, T., Nakamichi, J., Kasahara, T., Yajima and T., Kojima

Journal of Propulsion and Power Vol. 27 ( 3 ) page： pp. 597-607 2011

爆轟管同軸回転バルブを用いたパルスデトネーションエンジンの性能評価 Reviewed

中道達也, 松岡健, 笠原次郎, 松尾亜紀子, 船木一幸

航空宇宙技術 Vol. 10 page： pp. 107-112 2011

Combustion Wave Propagation and Detonation Initiation in the Vicinity of Closed-Tube End Walls Reviewed

J., Yageta, S., Shimada, K., Matsuoka, J., Kasahara and A., Matsuo

Proceedings of the Combustion Institute Vol. 33 page： pp. 2303-2310 2011

パルスデトネーションエンジン用入口流体駆動バルブに関する研究 Reviewed

山口敬之, 松岡健, 八桁純, 笠原次郎

日本航空宇宙学会論文集 Vol. 57 ( 663 ) page： pp.141-147 2009

Numerical Study for Hysteresis Phenomena of Shock Wave Reflection in Over-expanded Axisymmetric Supersonic Jet Reviewed

T. Yasunobu, K. Matsuoka, H. Kashimura, T. Setoguchi

Journal of Thermal Science Vol. 15 ( 3 ) page： pp.220-225 2006

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Papers - MATSUOKA Ken