トップページ  > 教員個別情報  > 論文 等

静岡大学教員データベース - 教員個別情報 : 川﨑 央 (KAWASAKI Akira)

論文 等

【論文 等】
[1]. Combustion Structure of a Cylindrical Rotating Detonation Engine with Liquid Ethanol and Nitrous Oxide Combustion and Flame
Combustion and Flame / - (2024年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Tomoki Sato, Kotaro Nakata, Kazuki Ishihara, Noboru Itouyama, Ken Matsuoka, Jiro Kasahara, Dr. Eng, Akira Kawasaki, Daisuke Nakata, Hikaru Eguchi, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki
[2]. Experimental demonstration on detonation initiation by laser ignition and shock focusing in elliptical cavity
Shock Waves 33/7-8 521-531 (2023年) [査読] 有
[責任著者・共著者の別]
[著者] T. Sato, K. Matsuoka, A. Kawasaki, N. Itouyama, H. Watanabe, J. Kasahara [URL]
[3]. Lagrangian dispersion and averaging behind a two-dimensional gaseous detonation front
Journal of Fluid Mechanics 968/ - (2023年) [査読] 有
[責任著者・共著者の別]
[著者] Hiroaki Watanabe, Akiko Matsuo, Ashwin Chinnayya, Noboru Itouyama, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara [URL]
[4]. Impact of mixture mass flux on hydrodynamic blockage ratio and Mach number of rotating detonation combustor
Acta Astronautica / - (2023年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Tomoyuki Noda, Ken Matsuoka, Keisuke Goto, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Jiro Kasahara, Akiko Matsuo
[5]. Numerical investigation of the effects of injector configuration on flow structures in annular and cylindrical rotating detonation combustors
Science and Technology of Energetic Materials 84/2 17-23 (2023年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Takumi Sada, Akiko Matsuo, Eiji Shima, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara
[6]. Visualization and Performance Evaluation of a Liquid-Ethanol Cylindrical Rotating Detonation Combustor
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 66/2 46-58 (2023年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Kazuki ISHIHARA, Kentaro YONEYAMA, Tomoki SATO, Hiroaki WATANABE, Noboru ITOUYAMA, Akira KAWASAKI, Ken MATSUOKA, Jiro KASAHARA, Akiko MATSUO, Ikkoh FUNAKI [URL]
[7]. Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine
Journal of Propulsion and Power / 1-11 (2023年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Kazuki Ishihara, Kentaro Yoneyama, Hiroaki Watanabe, Noboru Itouyama, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Kazuyuki Higashino [URL]
[8]. 宇宙飛行実証用デトネーションエンジンシステム制御・計測装置の開発
日本航空宇宙学会誌 70/12 256-262 (2022年) [査読] 有
[責任著者・共著者の別]
[著者] 松山 行一, 笠原 次郎, 川﨑 央, MATSUYAMA Koichi, KASAHARA Jiro, KAWASAKI Akira
[9]. 観測ロケットS-520-31号機によるデトネーションエンジン作動実証プロジェクトの総括
日本航空宇宙学会誌 70/11 224-233 (2022年) [査読] 有
[責任著者・共著者の別]
[著者] 松岡 健, 後藤 啓介, ブヤコフ バレンティン, 松山 行一, 川﨑 央, 伊東山 登, 渡部 広吾輝, 石原 一輝, 野田 朋之, 笠原 次郎, 松尾 亜紀子, 船木 一幸, 中田 大将, 内海 政春, 羽生 宏人, 竹内 伸介, 荒川 聡, 増田 純一, 前原 健次, 中尾 達郎, 山田 和彦, MATSUOKA Ken, GOTO Keisuke, BUYAKOFU Valentin, MATSUYAMA Koichi, KAWASAKI Akira, ITOUYAMA Noboru, WATANABE Hiroaki, ISHIHARA Kazuki, NODA Tomoyuki, KASAHARA Jiro, MATSUO Akiko, FUNAKI Ikkoh, NAKATA Daisuke, UCHIUMI Masaharu, HABU Hiroto, TAKEUCHI Shinsuke, ARAKAWA Satoshi, MASUDA Junichi, MAEHARA Kenji, NAKAO Tatsuro, YAMADA Kazuhiko
[10]. Experimental study on detonation-diffraction reflection point distances in hydrogen and gaseous hydrocarbon reactive systems
Combustion and Flame 245/ - (2022年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Han Sun, Akira Kawasaki, Noboru Itouyama, Ken Matsuoka, Jiro Kasahara [URL]
[11]. Experimental investigation of inner flow of a throatless diverging rotating detonation engine
Proceedings of the Combustion Institute / - (2022年) [査読] 有 [国際共著論文] 該当する
[責任著者・共著者の別] 共著者
[著者] Kotaro Nakata, Kazuki Ishihara, Keisuke Goto, Noboru Itouyama, Hiroaki Watanabe, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Kazuyuki Higashino, James Braun, Terrence Meyer, Guillermo Paniagua
[12]. Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31
Journal of Spacecraft and Rockets 60/1 273-285 (2022年) [査読] 有
[責任著者・共著者の別]
[著者] Keisuke Goto, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Kazuki Ishihara, Valentin Buyakofu, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao, Kazuhiko Yamada [URL]
[13]. Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space
Journal of Spacecraft and Rockets / 1-9 (2022年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao, Kazuhiko Yamada [URL]
[14]. Supersonic Exhaust from a Rotating Detonation Engine with Throatless Diverging Channel
AIAA Journal 60/7 4015-4023 (2022年) [査読] 有 [国際共著論文] 該当する
[責任著者・共著者の別] 共著者
[著者] Kotaro Nakata, Kosei Ota, Shiro Ito, Kazuki Ishihara, Keisuke Goto, Noboru Itouyama, Hiroaki Watanabe, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Kazuyuki Higashino, James Braun, Terrence Meyer, Guillermo Paniagua [URL]
[15]. Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket
Journal of Spacecraft and Rockets 59/3 850-860 (2022年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara [URL]
[16]. Cylindrical Rotating Detonation Engine with Propellant Injection Cooling
Journal of Propulsion and Power 38/3 410-420 (2022年) [査読] 有
[責任著者・共著者の別]
[著者] Keisuke Goto, Kosei Ota, Akira Kawasaki, Noboru Itouyama, Hiroaki Watanabe, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Hideto Kawashima [URL]
[17]. Investigation of reflective shuttling detonation cycle by schlieren and chemiluminescence photography
Combustion and Flame 236/ 111826-111826 (2022年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Tomoya Taguchi, Masato Yamaguchi, Ken Matsuoka, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Jiro Kasahara [URL]
[18]. Torque Around Axial Direction on Rotating Detonation Engines
Journal of Propulsion and Power 38/1 59-70 (2022年) [査読] 有 [国際共著論文] 該当しない
[責任著者・共著者の別] 共著者
[著者] Satoru Sawada, Keisuke Goto, Kazuki Ishihara, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki [URL]
[19]. Cathode temperature measurement of a hydrogen self-field MPD thruster during 1 ms quasi-steady operation
Journal of Applied Physics 130/17 173306-173306 (2021年) [査読] 有
[責任著者・共著者の別]
[著者] Yuya Oshio, Shitan Tauchi, Akira Kawasaki, Ikkoh Funaki [URL]
[20]. Investigation into the effective injector area of a rotating detonation engine with impact of backflow
Shock Waves / - (2021年) [査読] 有
[責任著者・共著者の別]
[著者] K. Goto, R. Yokoo, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Kawashima [URL]
[21]. Experimental investigation on a rotating detonation cycle with burned gas backflow
Combustion and Flame 225/ 13-19 (2021年) [査読] 有
[責任著者・共著者の別]
[著者] Ken Matsuoka, Masaya Tanaka, Tomoyuki Noda, Akira Kawasaki, Jiro Kasahara
[22]. Experimental study of internal flow structures in cylindrical rotating detonation engines
Proceedings of the Combustion Institute 38/3 3759-3768 (2021年) [査読] 有
[責任著者・共著者の別]
[著者] Yokoo, R., Goto, K., Kasahara, J., Athmanathan, V., Braun, J., Paniagua, G., Meyer, T.R., Kawasaki, A., Matsuoka, K., Matsuo, A., Funaki, I.
[23]. Numerical analysis on behavior of dilute water droplets in detonation
PROCEEDINGS OF THE COMBUSTION INSTITUTE 38/3 3709-3716 (2021年) [査読] 有
[責任著者・共著者の別]
[著者] Hiroaki Watanabe, Akiko Matsuo, Ashwin Chinnayya, Ken Matsuoka, Akira Kawasaki, Jiro Kasahara
[24]. Investigation of combustion modes and pressure of reflective shuttling detonation combustor
Proceedings of the Combustion Institute 38/3 3615-3622 (2021年) [査読] 有
[責任著者・共著者の別]
[著者] Masato Yamaguchi, Tomoya Taguchi, Ken Matsuoka, Akira Kawasaki, Jiro Kasahara, Hiroaki Watanabe, Akiko Matsuo
[25]. A study on detonation-diffraction reflection point distances in H2/O2, C2H2/O2, and C2H4/O2systems
Proceedings of the Combustion Institute 38/3 3605-3613 (2021年) [査読] 有
[責任著者・共著者の別]
[著者] Sun, H., Kawasaki, A., Matsuoka, K., Kasahara, J. [URL]
[26]. Propulsion Performance of Cylindrical Rotating Detonation Engine
AIAA JOURNAL 58/12 5107-5116 (2020年) [査読] 有
[責任著者・共著者の別]
[著者] Ryuya Yokoo, Keisuke Goto, Juhoe Kim, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki
[27]. Numerical analysis of the mean structure of gaseous detonation with dilute water spray
Journal of Fluid Mechanics 887/ - (2020年) [査読] 有
[責任著者・共著者の別]
[著者] Hiroaki Watanabe, Akiko Matsuo, Ashwin Chinnayya, Ken Matsuoka, Akira Kawasaki, Jiro Kasahara [URL]
[28]. Optical Measurement of Fluid Motion in Semi-Valveless Pulse Detonation Combustor with High-Frequency Operation
COMBUSTION SCIENCE AND TECHNOLOGY 192/2 197-212 (2020年) [査読] 有
[責任著者・共著者の別]
[著者] Akiya Kubota, Ken Matsuoka, Akira Kawasaki, Jiro Kasahara, Hiroaki Watanabe, Akiko Matsuo, Takuma Endo [URL]
[29]. A novel characteristic length of detonation relevant to supercritical diffraction
Shock Waves 30/1 1-12 (2020年) [査読] 有
[責任著者・共著者の別]
[著者] A. Kawasaki, J. Kasahara [URL]
[30]. Investigation of the measurement characteristics of a multiple-ion-probe method for a propagating methane-oxygen-nitrogen flame
COMBUSTION AND FLAME 211/ 112-123 (2020年) [査読] 有
[責任著者・共著者の別]
[著者] Tomoaki Yatsufusa, Keigo Kii, Naoya Miura, Hiroki Yamamoto, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara
[31]. Semi-valveless pulse detonation cycle at a kilohertz-scale operating frequency
COMBUSTION AND FLAME 205/ 434-440 (2019年) [査読] 有
[責任著者・共著者の別]
[著者] Ken Matsuoka, Haruna Taki, Akira Kawasaki, Jiro Kasahara, Hiroaki Watanabe, Akiko Matsuo, Takuma Endo
[32]. Numerical investigation on propagation behavior of gaseous detonation in water spray
PROCEEDINGS OF THE COMBUSTION INSTITUTE 37/3 3617-3626 (2019年) [査読] 有
[責任著者・共著者の別]
[著者] Hiroaki Watanabe, Akiko Matsuo, Ken Matsuoka, Akira Kawasaki, Jiro Kasahara
[33]. Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor
PROCEEDINGS OF THE COMBUSTION INSTITUTE 37/3 3741-3747 (2019年) [査読] 有
[責任著者・共著者の別]
[著者] Masato Yamaguchi, Ken Matsuoka, Akira Kawasaki, Jiro Kasahara, Hiroaki Watanabe, Akiko Matsuo
[34]. Critical condition of inner cylinder radius for sustaining rotating detonation waves in rotating detonation engine thruster
PROCEEDINGS OF THE COMBUSTION INSTITUTE 37/3 3461-3469 (2019年) [査読] 有
[責任著者・共著者の別]
[著者] Akira Kawasaki, Tomoya Inakawa, Jiro Kasahara, Keisuke Goto, Ken Matsuoka, Akiko Matsuo, Ikkoh Funaki
[35]. 臨界電流における水素MPDスラスタのプラズマ挙動に関する数値解析
日本航空宇宙学会論文集 67/5 159-166 (2019年) [査読] 有
[責任著者・共著者の別]
[著者] 田内 思担, 川﨑 央, 中根 昌克, 窪田 健一, 船木 一幸, Shitan Tauchi, Akira Kawasaki, Masakatsu Nakane, Kenichi Kubota, Ikkoh Funaki [URL]
[36]. Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles
JOURNAL OF PROPULSION AND POWER 35/1 213-223 (2019年) [査読] 有
[責任著者・共著者の別]
[著者] Keisuke Goto, Junpei Nishimura, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Kazuyuki Higashino [URL]
[37]. The Effect of Anode Configuration on Hydrogen MPD Thruster Performance: A Numerical Study
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 16/3 274-279 (2018年) [査読] 有
[責任著者・共著者の別]
[著者] Shitan TAUCHI, Akira KAWASAKI, Masakatsu NAKANE, Kenichi KUBOTA, Ikkoh FUNAKI [URL]
[38]. MPDスラスタ内の放電電流経路と推進性能に関する数値的検討
電気学会論文誌A(基礎・材料・共通部門誌) 136/3 135-140 (2016年) [査読] 有
[責任著者・共著者の別]
[著者] 川﨑 央, 窪田 健一, 船木 一幸, 奥野 喜裕, Kawasaki Akira, Kubota Kenichi, Funaki Ikkoh, Okuno Yoshihiro [URL]
[39]. 水素MPDスラスタの放電電流経路に関する数値的検討
電気学会論文誌A(基礎・材料・共通部門誌) 136/3 141-146 (2016年) [査読] 有
[責任著者・共著者の別]
[著者] 川﨑 央, 窪田 健一, 船木 一幸, 奥野 喜裕, Kawasaki Akira, Kubota Kenichi, Funaki Ikkoh, Okuno Yoshihiro [URL]
[40]. MHD Simulation and Thermal Design of an MPD Thruster
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 12/ists29 Pb_19-Pb_25 (2014年) [査読] 有
[責任著者・共著者の別]
[著者] KAWASAKI Akira, KUBOTA Kenichi, FUNAKI Ikkoh, OKUNO Yoshihiro, Akira KAWASAKI, Kenichi KUBOTA, Ikkoh FUNAKI, Yoshihiro OKUNO [URL]
[41]. 数値計算による自己誘起磁場型アルゴンMPDスラスタの熱設計
日本航空宇宙論文集 61/6 167-173 (2013年) [査読] 有
[責任著者・共著者の別]
[著者] 川﨑 央, 窪田 健一, 船木 一幸, 奥野 喜裕, Akira KAWASAKI, Kenichi KUBOTA, Ikkoh FUNAKI, Yoshihiro OKUNO [URL]