Faculty Profiles - MATSUOKA Ken

Papers - MATSUOKA Ken

Division display 41 - 60 of about 64 ／ All the affair displays >>

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

　 PREV - NEXT 　

<MATSUOKA Ken>

Papers - MATSUOKA Ken