J. Kasahara, Y. Kato, K. Ishihara, K. Goto, K. Matsuoka, A. Matsuo, I. Funaki, H. Moriai, D. Nakata, K. Higashino, N. Tanatsugu, pp.61-76, Chapter 4, Application of Detonation Waves to Rocket Engine Chamber, Detonation Control for Propulsion, Pulse Detonation and Rotating Detonation Engines, Springer, 2018.
K. Matsuoka, H. Taki, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, pp.183-198, Chapter 8, Pulse Detonation Cycle at Kilohertz Frequency, Detonation Control for Propulsion, Pulse Detonation and Rotating Detonation Engines, Springer, 2018.
笠原次郎、前田慎市、遠藤琢磨、笠原裕子(訳)、J. H. S. Lee(著)、デトネーション現象、化学工業日報社、2018.2.
K. Ishihara, K. Yoneyama, T. Sato, H. Watanabe, N. Itouyama, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I., Funaki, Visualization and Performance Evaluation of Liquid-Ethanol Cylindrical Rotating Detonation Combustor, Transaction of JSASS Aerospace Technology Japan (Accepted for publication, 22th November, 2022)
K. Ishihara, K. Yoneyama, H. Watanabe, N. Itouyama, K. Akira, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, K. Higashino, Evaluation of Thrust Performance of Converging Rotating Detonation Engine, Journal of Propulsion and Power (accepted 15th January 2022)
H. Sun, A. Kawasaki, N. Itouyama, K. Matsuoka, J. Kasahara, Experimental Study on Detonation-Diffraction Reflection Point Distances in Hydrogen and Gaseous Hydrocarbon Reactive Systems, Combustion and Flame (published 7th September 2022)
https://doi.org/10.1016/j.combustflame.2022.112329
K. Goto, K. Matsuoka, K. Matsuyama, A. 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, Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31, Journal of Spacecraft and Rocket (Published online 25th October,2022)
https://arc.aiaa.org/doi/10.2514/1.A35401
V. Buyakofu, K. Matsuoka, K. Matsuyama, A. 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, Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space, Journal of Spacecraft and Rocket (online published 1st September,2022) https://arc.aiaa.org/doi/10.2514/1.A35394
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, Experimental investigation of inner flow of a throat less diverging rotating detonation engine, Proceedings of the Combustion Institute (Accepted for publication on August 10th, 2022)
K. Nakata, K. Ota, S. Ito, K. Ishihara, K. Goto, I. Noboru, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, K. Higashino, J. Braun, T. Meyer, G. Paniagua, Supersonic Exhaust from a Rotating Detonation Engine with Throatless Diverging Channel, AIAAJ, Vol 60, No.7 (2022), pp. 4015-4023.
http://arc.aiaa.org/doi/abs/10.2514/1.J061300
V. Buyakofu, K. Matsuoka, K. Matsuyama, A. 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, Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket, Journal of Spacecraft and Rocket (published online 3rd January, 2022). https://arc.aiaa.org/doi/10.2514/1.A35200
K. Goto, K. Ota, A. Kawasaki, N. Itouyama, H. Watanabe, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Kawashima, Cylindrical Rotating Detonation Engine with Propellant Injection Cooling, Journal of Propulsion and Power, Vol.38, No.3, 2022, pp.410-420 https://doi.org/10.2514/1.B38427
T, Taguchi, M. Yamaguchi, K. Matsuoka, A. Kawasaki, H. Watanabe, J. Kasahara, A. Matsuo, Investigation of Reflective Shutting Detonation Cycle by Schlieren and Chemiluminescence Photography, Combustion and Flame (published online 2nd November, 2021) https://doi.org/10.1016/j.combustflame.2021.111826
S. Sawada, K. Goto, K. Ishihara, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of Torque Around the Axial Direction on Rotating Detonation Engines, Journal of Propulsion and Power, Vol. 38, No.1, 2022, pp. 59-70. https://doi.org/10.2514/1.B38374
K. Goto, R. Yokoo, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Kawashima, Investigation of the Effective Injector Area of a Rotating Detonation Engine with Impact of Backflow, Shock Waves, Vol.31, 2021, pp.753-762. http://link.springer.com/article/10.1007/s00193-021-00998-9
K. Goto, Y. Kato, K. Ishihara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, K. Higashino, and N. Tanatsugu, Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled-Test, Journal of Propulsion and Power,Vol.37, No. 3, 2021, pp.419-425 http://arc.aiaa.org/doi/abs/10.2514/1.B38037
K. Matsuoka, M. Tanaka, T. Noda, A. Kawasaki, J. Kasahara, Experimental Investigation on a Rotating Detonation Cycle with Backflow of Burned Gas,Combustion and Flame, Vol.225, 2021, pp.13-19. https://doi.org/10.1016/j.combustflame.2020.10.048
R. Yokoo, K. Goto, J. Kasahara, V. Athmanathan, J. Braun, G. Paniagua, T. Meyer, A. Kawasaki, K. Matsuoka, A. Matsuo, I. Funaki, Experimental Study of Internal Flow Structures in Cylindrical Rotating Detonation Engines, Proceedings of the Combustion Institute, Vol.38, No. 3, 2021, pp.3759-3768.. https://doi.org/10.1016/j.proci.2020.08.001
H. Sun, A. Kawasaki, K. Matsuoka, J. Kasahara, A Study on Detonation-Diffraction Reflection Point Distances in H2/O2, C2H2/O2, and C2H4/O2 Systems, Proceedings of the Combustion Institute, Vol.38, No. 3, 2021, pp.3605-3613. https://doi.org/10.1016/j.proci.2020.06.371
M. Yamaguchi, K. Matsuoka, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, Investigation of combustion modes and pressure of reflective shuttling detonation combustor, Proceedings of the Combustion Institute, Vol.38, No. 3, 2021, pp.3615-3622. https://doi.org/10.1016/j.proci.2020.07.064
H. Watanabe, A. Matsuo, A. Chinnayya, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical Analysis on Behavior of Dilute Water Droplets in Detonation, Proceedings of the Combustion Institute, Vol.38, No. 3, 2021, pp.3709-3716. https://doi.org/10.1016/j.proci.2020.07.141
H. Watanabe, A. Matsuo, Akiko, A. Chinnayya, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical Analysis of the Mean Structure of Gaseous Detonation with Dilute Water Spray, Journal of Fluid Mechanics, Vol.887, A4, 2020,https://doi.org/10.1017/jfm.2019.1018
R. Yokoo, K. Goto, J. Kim, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Propulsion Performance of Cylindrical Rotating Detonation Engine, AIAA Journal , Vol. 58, No. 12, 2020, pp.5107-5116. http://arc.aiaa.org/doi/abs/10.2514/1.J058322
T. Yatsufusa, K. Kii, N. Miura, H. Yamamoto, A. Kawasaki, K. Matsuoka, J. Kasahara, Investigation of the Measurement Characteristics of a Multiple-Ion-Probe Method for a Propagating Methane–Oxygen–Nitrogen Flame, Combustion and Flame, Vol.211, 2020, pp.112-123. https://doi.org/10.1016/j.combustflame.2019.09.022
K. Matsuoka, H., Taki, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, and T. Endo, Semi-Valveless Pulse Detonation Cycle at a Kilohertz-scale Operating Frequency, Combustion and Flame, Vol. 205, 2019, pp. 434-440. DOI: 10.1016/j.combustflame.2019.04.035
J. Shepherd, J. Kasahara, Analytical Models for the Thrust of a Rotating Detonation Engine, GALCIT Report FM2017.001,
A. Kawasaki, J. Kasahara, A Novel Characteristic Length of Detonation Relevant to Supercritical Diffraction, Shock Waves, Vol.30, No.1, 2020, pp.1-12. DOI: 10.1007/s00193-019-00890-7 https://doi.org/10.1007/s00193-019-00890-7
A. Kubota, K. Matsuoka, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, and T. Endo, Optical Measurement of Fluid Motion in Semi-Valveless Pulse Detonation Combustor with High-Frequency Operation, Combustion Science and Technology, Vol. 192, 2020, pp.197-212.DOI: 10.1080/00102202.2018.1559837
K. Goto, J. Nishimura, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, K. Higashino, Experimental Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Throat Geometries, Journal of Propulsion and Power, Vol. 35, No. 1, 2019, pp.213-223. DOI: 10.2514/1.B37196
A. Kawasaki, T. Inakawa, J. Kasahara, K. Goto, K. Matsuoka, A. Matsuo, I. Funaki, Critical Condition of Inner Cylinder Radius for Sustaining Rotating Detonation Waves in Rotating Detonation Engine Thruster, Proceedings of the Combustion Institute, Vol. 37, No. 3, 2019, pp. 3461-3469. DOI: 10.1016/j.proci.2018.07.070
M. Yamaguchi, K. Matsuoka, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, Study on a Reflective Shuttling Detonation Wave in Fan-Shaped Two-Dimensional Combustor, Proceedings of the Combustion Institute, Vol. 37, No. 3, 2019, pp. 3741-3747. DOI: 10.1016/j.proci.2018.06.210
H. Watanabe, A. Matsuo, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical Investigation on Propagation Behavior of Gaseous Detonation in Water Spary, Proceedings of the Combustion Institute, Vol. 37, No. 3, 2019, pp. 3617-3626. DOI: 10.1016/j.proci.2018.07.092
K. Matsuoka, S. Takagi, J. Kasahara, A. Matsuo, T. Endo, Validation of Pulse Detonation Operation in Low-Ambient-Pressure Environment Journal of Propulsion and Power, Vol. 34, No. 1, 2018, pp.116-124. DOI: 10.2514/1.B36401
S. Nakagami, K. Matsuoka, J. Kasahara, Y. Kumazawa, J. Fujii, A. Matsuo, I. Funaki, Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor, Journal of Propulsion and Power, Vol. 33, No. 1, 2017, pp.80-88.
K. Matsuoka, K. Muto, J. Kasahara, H. Watanabe, A. Matsuo and T. Endo, Development of High-Frequency Pulse Detonation Combustor without Purging Material, Journal of Propulsion and Power, Vol. 33, No. 1, 2017, pp.43-50.
S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of the Structure of Forward-Tilting Rotating Detonation Waves and Highly Maintained Combustion Chamber Pressure in a Disk-Shaped Combustor, Proceedings of the Combustion Institute, Vol. 36, No. 2, 2017, pp. 2673-2680.
K. Matsuoka, K. Muto, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, Investigation of Fluid Motion in Valveless Pulse Detonation Combustor with High-Frequency Operation, Proceedings of the Combustion Institute, Vol. 36, No. 2, 2017, pp. 2641-2647.
J. Fujii, Y. Kumazawa, A. Matsuo, S. Nakagami, J. Kasahara, Numerical Investigation on Velocity Deficit of Detonation Wave in RDE Chamber, Proceedings of the Combustion Institute, Vol. 36, No. 2, 2017, pp. 2665-2672.
Y. Nagura, J. Kasahara, A. Matsuo, Multi-Frame Visualization for Detonation Wave Diffraction, Shock Waves, Vol. 26, No. 5, 2016, pp.645-656.
K. Matsuoka, T. Morozumi, S. Takagi, J. Kasahara, A. Matsuo, I. Funaki, Flight Validation of a Rotary-Valved Four-Cylinder Pulse Detonation Rocket, Journal of Propulsion and Power, Vol. 32, No. 2, 2016, pp.383-391.
H. Yamada, Y. Yamagishi, H. Sakakita, S. Tsunoda, J. Kasahara, M. Fujiwara, S. Kato, H. Itagaki, J. Kim, S. Kiyama, Y. Fujiwara, Y. Ikehara, S. Ikehara, H. Nakanishi, and N. Shimizu, Turbulent enhancement and flow control of a neutral gas containing an atmospheric pressure plasma, Japanese Journal of Applied Physics, Vol. 55, 01AB08, 2016.
K. Matsuoka, R. Sakamoto, T. Morozumi, J. Kasahara, A. Matsuo, I. Funaki, Thrust Performance of Rotary-Valved Four-Cylinder Pulse Detonation Rocket Engine, Transaction of the Japan Society for Aeronautical and Space Sciences, Vol. 58, No. 4, pp. 193-203, 2015.
S. Maeda, S. Sumiya, J. Kasahara, A. Matsuo, Scale Effect of Spherical Projectiles for Stabilization of Oblique Detonation Waves, Shock Waves, Vol. 25, 2015, pp. 141-150.
Y. Sugiyama, A. Matsuo, H. Nakayama, and J. Kasahara, Numerical Investigations on Detonation Propagation in a Two-Dimensional Curved Channel, Combustion Science and Technology, Vol. 186, 2014, 1662・679.
Y. Nagura, J. Kasahara, Y. Sugiyama, and A. Matsuo, Comprehensive Visualization of Detonation-Diffraction Structures and Sizes in Unstable and Stable Mixtures, Proceedings of the Combustion Institute, Vol. 34, 2013, pp.1949-1956.
H. Nakayama, J. Kasahara, A. Matsuo, and I. Funaki, Front shock behavior of stable curved detonation waves in rectangular-cross-section curved channels, Proceedings of the Combustion Institute, Vol. 34, 2013, pp.1939-1947.
S. Maeda, S. Sumiya, J. Kasahara, and A. Matsuo, Initiation and Sustaining Mechanisms of Stabilized Oblique Detonation Waves around Projectiles, Proceedings of the Combustion Institute, Vol. 34, 2013, pp.1973-1980.
H. Yamashita, J. Kasahara, Y. Sugiyama, and A. Matsuo, Visualization Study of Ignition Modes Behind Bifurcated-Reflected Shock Waves, Combustion and Flame, Vol. 159, 2012, No. 9, pp.2954-2966.
H. Nakayama, T. Moriya, J. Kasahara, A. Matsuo, Y. Sasamoto, and I. Funaki, Propagation of Curved Detonation Waves Stabilized in Annular Channels, Transaction of JSASS Aerospace Technology Japan, 10, ists28, Pe_7-14 (2012)
K. Matsuoka, M. Esumi, K. B. Ikeguchi, J. Kasahara, A. Matsuo, and I. Funaki, Experimental Investigation of a Multi-Cycle Single Tube Pulse Detonation Rocket Engine with a Coaxial Rotary Valve, Transaction of JSASS Aerospace Technology Japan, 10, ists28, Te_1-4 (2012)
S. Maeda, J. Kasahara, A. Matsuo, Unsteady Propagation Process of Oblique Detonation Waves Initiated by Hypersonic Projectiles, Transaction of JSASS Aerospace Technology Japan, 10, ists28, Pe_1-6 (2012)
K. Matsuoka, M. Esumi, K. B. Ikeguchi, J. Kasahara, A. Matsuo, and I. Funaki, Optical and Thrust Measurement of a Pulse Detonation Combustor with a Coaxial Rotary Valve, Combustion and Flame, Vol. 159, 2012, No. 3, pp.1321-1338.
S. Maeda, J. Kasahara, and A. Matsuo, Oblique Detonation Wave Stability Around a Spherical Projectile by a High Time Resolution Optical Observation, Combustion and Flame, Vol. 159, 2012, No. 2, pp.887-896.
H. Nakayama, T. Moriya, J. Kasahara, A. Matsuo, Y. Sasamoto, and I. Funaki, Stable Detonation Wave Propagation in Rectangular-Cross-Section Curved Channels, Combustion and Flame, Vol. 159, 2012, No. 2, pp.859-869.
中道達也,松岡健,笠原次郎,松尾亜紀子,船木一幸,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,航空宇宙技術,Vol. 10, 2011, pp. 107-112.
K. Kawane, S. Shimada, J. Kasahara, and A. Matsuo, The Influence of Heat Transfer and Friction on the Impulse of a Detonation Tube, Combustion and Flame , Vol. 158, No. 10, 2011, pp.2023-2036.
K. Matsuoka, J. Yageta, T. Nakamichi, J. Kasahara, T. Yajima, T. Kojima, !nflow-Driven Valve System for Pulse Detonation Engines, Journal of Propulsion and Power, Vol. 27, No.3, May-June 2011, pp.597-607.
Y. Kudo, Y. Nagura, J. Kasahara, Y. Sasamoto, A. Matsuo, Oblique Detonation Waves Stabilized in Rectangular-Cross-Section Bent Tubes, Proceedings of the Combustion Institute, Vol.33, 2011, pp.2319-2326
S. Maeda, R. Inada, J. Kasahara, A. Matsuo, Visualization of the Non-Steady State Oblique Detonation Wave Phenomena around Hypersonic Spherical Projectile, Proceedings of the Combustion Institute, Vol. 33, 2011, pp.2343-2349
J. Yageta, S. Shimada, K. Matsuoka, J. Kasahara, A. Matsuo, Combustion Wave Propagation and Detonation Initiation in the Vicinity of Closed-Tube End Walls, Proceedings of the Combustion Institute, Vol. 33, 2011, pp.2303-2310
S. Kato, S. Hashimoto, A. Uemichi, J. Kasahara, A. Matsuo, Propagation Characteristics of Shock Waves Driven by Gaseous Detonation Waves, Shock Waves, Vol. 20, No.6, 2010, pp.479-489
S. Maeda, J. Kasahara, A. Matsuo, T. Endo, Analysis on Thermal Efficiency of Non-Compressor Type Pulse Detonation Turbine Engine, Transaction of the Japan Society for Aeronautical and Space Sciences, Vol.53, No.181, 2010, pp.192-206
J. Kasahara, M. Hirano, A. Matsuo, Y. Daimon, T. Endo, Thrust Measurement of a Multicycle Partially Filled Pulse Detonation Rocket Engine, Journal of Propulsion and Power, Vol.25, No.6, November-December 2009, pp.1281-1290
J. Kasahara, A. Hasegawa, T. Nemoto, H. Yamaguchi,T. Yajima , T. Kojima, Performance Validation of a Single-Tube Pulse Detonation Rocket System, Journal of Propulsion and Power, Vol.25, No.1, January-February 2009, pp.173-180
J. Kasahara, Z. Liang, S. T. Browne, and J. E. Shepherd, Impulse Generation by an Open Shock Tube, AIAA Journal, Vol.46, No. 7, 2008, pp.1593-1603
T. Endo, T. Yatsufusa, S. Taki, A. Matsuo, K. Inaba, and J. Kasahara, Homogeneous-Dilution Model of Partially Fueled Simplified Pulse Detonation Engines, Journal of Propulsion and Power, Vol.23, No.5, 2007, pp.1033-1041
T. Fujino, Y. Matsumoto, J. Kasahara, and M. Ishikawa, Numerical Studies of Magnetohydrodynamic Flow Control Considering Real Wall Electrical Conductivity, Journal of Spacecraft and Rocket, Vol.44, No.3, May-June, 2007, pp. 625-632
S. Sato, A. Matsuo, T. Endo, J. Kasahara,Numerical Studies on Specific Impulse of Partially Filled Pulse Detonation Rocket Engines, Journal of Propulsion and Power, Vol. 22, No. 1, 2006, pp.64-69
遠藤琢磨,八房智顕,滝史郎,笠原次郎,パルスデトネーションタービンエンジンの性能に関する熱力学的解析,Science and Technology of Energetic Materials, Vol.65, No.4, 2004,7月-8月, pp.103-110
T. Endo, J. Kasahara, A. Matsuo, K. Inaba, S. Sato, T. Fujiwara, Pressure History at the Thrust Wall of a Simplified Pulse Detonation Engine, AIAA Journal, Vol. 42, No. 9, 2004, pp.1921-1930
F. Sakima, T. Arai, J. Kasahara, M. Murakoshi, T. Ami, F. He, H. Sugiyama, Mixing of a Hydrogen Jet from a Wedge Shaped Injector into a Supersonic Cross Flow, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 46, No. 154, 2004, pp.217-223
J. Kasahara, K. Takazawa, T. Arai, Y. Tanahashi, S. Chiba, and A. Matsuo, Experimental Investigations of Momentum and Heat Transfer in Pulse Detonation Engines, Proceedings of the Combustion Institute, Vol. 29, 2002, pp.2847-2854
J. Kasahara, T. Arai, S. Chiba, K. Takazawa, Y. Tanahashi, and A. Matsuo, Criticality for Stabilized Oblique Detonation Waves Around Spherical Bodies in Acetylene/Oxygen/Krypton Mixtures, Proceedings of the Combustion Institute, Vol. 29, 2002, pp.2817-2824
J. Kasahara, T. Fujiwara, T. Endo, T. Arai, Chapman-Jouguet Oblique Detonation Structure Around Hypersonic Projectiles, AIAA Journal, Vol. 39, No. 8, 2001, pp.1553-1561
J. Kasahara, T. Endo, K. Nishide, D. Yahata, T. Fujiwara and J. E. Leblanc, Experimental Study of Interaction between Oblique Detonation and Rarefaction Wave Around a Hypersonic Free Projectile, Journal de Physique IV, Vol.10, 2000, Pr11-pp.109-115
堀井孝浩,笠原次郎,遠藤琢磨,藤原俊隆,極超音速飛行体周りにおけるCO-O2-H2予混合気体の非定常燃焼に関する実験的研究,日本機械学会論文集(B編),63巻,607号,1997,pp.917-924 (翻訳) T. Horii, J. Kasahara, T. Endo and T. Fujiwara, Experimental Studies on Supersonic Combustion Phenomena of CO-O2-H2 Premixed Gases Around Hypersonic Projectiles,JSME International Journal, Series B, Vol. 41, No.2, 1998, pp.316-321
J. Kasahara, T. Horii, T. Endo, and T. Fujiwara, Experimental Observation of Unsteady H2-O2 Combustion Phenomena Around Hypersonic Projectiles Using a Multiframe Camera, Symposium (International) on Combustion, Vol. 26, 1996, pp.2903-2908
K. Komurasaki, J. Kasahara, S. Yano, and T. Fujiwara, Radiation in a Hypersonic Shock Layer Generated Around a Projectile, Shock Waves, Vol.5, 1995,pp.217-22
J. Kasahara, Detonation Fluid Dynamics Phenomena and Its Application to Aerospace Propulsion, ICFD2022, Sendai, Japan, 10th November, 2022(受賞記念講演).
J. Kasahara, Flight Experiment of Detonation Engine System By Using Sounding Rocket S-520-31 and Future Flight Experiments, 2022 Silk Road International Conference on the Cooperation and Integration of Industry, Education, Research and Application, 9th November 2022, Xian, China.
J. Kasahara, Fundamental Research of Detonation Engine and Its Space Flight Experiment Using Sounding Rocket, (Plenary Lecture), 28th International Colloquium on the Dynamics of Explosions and Reactive Systems, June 19-24, 2022, Naples, Italy.
笠原次郎,デトネーションエンジンの観測ロケット宇宙飛行実験と今後の展開,日本衝撃波研究会Glass Memorial Lecture Award 受賞特別講演,2021年度衝撃波シンポジウム,日本衝撃波研究会,2022.3.10,立命館大学,滋賀,Online.
J. Kasahara, The Space Flight Experiment of Detonation Engine System Using The Sounding Rocket S-520-31, International Colloquium on Shock Waves, Australia, 2021. 12. 8. Virtual Event.
J. Kasahara, Challenges and Successes of Harnessing Detonation-Based Combustion for Propulsion Applications, Technical Panel, PDC-01, AIAA Propulsion and Energy, Aug. 9-11, 2021, Virtual Event.
J. Kasahara, Rocket Application and Sounding Rocket Experiment of Rotating Detonation Engine Technology, 10 th Internatinal Workshop on Detonation for Proulsion, September 9–11, 2019 in St. Petersburg, Russia.
J. Kasahara, Rotating and Pulse Detonation Engines System Development for the Sounding Rocket S520-31 Space Flight Experiment (Plenary Lecture), 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 28-August 2, 2019, Beijing, China.
J. Kasahara, Space flight demonstration of rotating and pulse detonation engines by sounding rocket S520-31 (Invited Overview), The 2nd International Workshop on Near Limit Flames, July 27-28, 2019, Peking University, Beijing, China.
J. Kasahara, Rotating Detonation (Lecture 4), Summer School on Detonation, July 27, 2019, Tsinghua University, Beijing, China.
J. Kasahara, Research and Development of Rotating Detonation Engone system for the Sounding Rocket Flight Experiment (keynote session, 基調講演セッション), The 8th BSME International Conference on Thermal Engineering, Dhaka, Bangladesh, 12-21 Dcember 2018.
J. Kasahara, Research of Rotating Detonation Engine for Space Flight System, Annual Conference of State Key Lab of Explosion Science and Technology & 2018 International Workshop on Intensive Loading and Its Effect, 30 November-2 December, Beijing China, 2018.
J. Kasahara, A. Kawasaki, K. Matsuoka, A. Matsuo I. Funaki D. Nakata, M. Uchiumi, Research and Development of Rotating Detonation Engine System for the Sounding Rocket Flight Experiment (keynote lecture, 基調講演), 11th International Colloquium on Pulsed and Continuous Detonations (ICPCD) to be held on September 17–21, 2018 in St. Petersburg, Russia.
J. Kasahara, A. Kawasaki, K. Matsuoka, A. Matsuo I. Funaki D. Nakata, M. Uchiumi, K. Higashono, Experimental Research of Rotating Detonation Engine System toward the Sounding Rocket S520 Space Flight, International Workshop on Detonation for Propulsion 2018, 10-13 September 2018, Xi’an, China.
J. Kasahara, Research and Development of Rotating Detonation Rocket Engine System for the Sounding Rocket Flight Experiment, The 50th KSPE Spring Conference, 31 May 2018, Jeju, Korea.
J. Kasahara, Study on Rotating Detonation Engine Performance for Sounding Rocket Experiments, 5th National symposium on Shock Waves, India, Feb 26-28, 2018.
J. Kasahara, K. Matsuoka, A. Kawasaki, K. Goto, J. Nishimura, J. Higashi, H. Taki, T. Ukai, Y. Hayamizu, K. Hiroyuki, T. Yamada, S. Watanabe, K. Hotta, T. Inakawa, Y. Kubota, M. Yamaguchi, T. Daicho, A. Matsuo, I. Funaki, K. Yasuda, K. Mori, H. Yagihashi, D. Nakata, M. Uchiumi, K. Higashino, Study on Rotating Detonation Engine Performance in Low Ambient Pressure for Sounding Rocket Flight Experiment, International Workshop on Detonation for Propulsion 2017, Poitiers, December 12-15, 2017.
J. Kasahara, Study on Rotating Detonation Engine Performance for Sounding Rocket Experiments, 5th National symposium on Shock Waves, India, Feb 26-28, 2018.
J. Kasahara, Experiments of Rotating Detonation Engines for Kick-Motors of Upper-Stage Rocket System (keynote speech, 基調講演), 27th National Conference on Combustion and Energy, Taiwan, April 21-22, 2017J. Kasahara, Experiments of Rotating Detonation Engines for Kick-Motors of Upper-Stage Rocket System (keynote speech, 基調講演), 27th National Conference on Combustion and Energy, Taiwan, April 21-22, 2017
J. Kasahara, Y. Kato, K. Ishihara, K. Goto, K. Matsuoka, A. Matsuo, I., Funaki, Research of Kick-Motor Rocket System of Rotating Detonation Engines(keynote speech, 基調講演), 10th International Colloquium on Pulsed and Continuous Detonations, St. Petersburg, Russia, July 4-8, 2016
J. Kasahara, Experimental Investigation of Rotating Detonation Engines for Sounding Rocket Flight Test System, International Workshop on Detonation for Propulsion 2016, Singapore, July 12-15, 2016
J. Kasahara, 500-N Class Rotating Detonation Rocket Engine Experiments, IWDP2015, Peking University, August 26-29, 2015, China.
J. Kasahara, 500-N Class Rotating Detonation Rocket Engine Experiment and Sounding Rocket Flight Test Program, Special Session: Rocket Applications of PGC, AIAA Propulsion and Energy Forum, July 27-29, 2015, Orlando US, (発表決定)
J. Kasahara, Present Status for Pulse and Rotating Detonation Engine Researches, 25th International Colloquium on the Dynamics of Explosions and Reactive Systems, August 2-7, 2015, Leeds, UK , (発表決定)
J. Kasahara, The Pulse Detonation Rocket Engine Flight Demonstrator “Todoroki II” and RDE Visualization Research, IWDP2014, Institute of Aviation, Warsaw, Poland, 22-24 June, 2014
J. Kasahara, Pulse Detonation Rocket Engine “Todoroki II” Flight Test and Rotating Detonation Engine Visualization, International Session ・Status of Pressure Gain Combustion for Propulsion, Research & Application I, AIAA SciTech2014, Maryland, US, 2014. January 15.
J. Kasahara, K. Matsuoka, R. Sakamoto, T. Morozumi, T., Kashiwazaki, Y. Fujiwara, A. Matsuo, I. Funaki, Experimental Study on a Four-Cylinder Pulse Detonation Rocket Engine Test Model, IWDP 2013, Tainan, Taiwan, 2013. July 26th-28th.
J. Kasahara, K. Matsuoka, M. Esumi, K. B. Ikeguchi, A. Matsuo, I. Funaki High-Frequency Rotary-Valve Pulse Detonation Rocket Engine Development, 2011 International Workshop on Detonation for Propulsion, Pusan National University, Busan, Korea, 2011.11.14-15
J. Kasahara, K. Matsuoka, T. Nakamichi, M. Esumi, A. Matsuo, I. Funaki, Study on High-Frequency Rotary-Valve Pulse Detonation Rocket Engines, Detonation Wave Propulsion Workshop, MBDA, Bourges, Subdray, France, 2011.7.11
J. Kasahara, K. Matsuoka, T. Nakamichi, M. Esumi, I. Funaki, A. Matsuo, 第2回デトネーション・デトネーションエンジンに関する会議、Study on Rotary-Valve Pulse Detonation Rocket Engine、北京昌平、中国、2011.5.14
A. Matsuo, Y. Sasamoto, J. Kasahara, H. Nakayama, 第2回デトネーション・デトネーションエンジンに関する会議、Curved Detonation in Bend Tube、北京昌平、中国、2011.5.14
釜山大学 2010
Papers presented at international conferences 国際会議発表論文
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, Experimental Investigation of Innner Flow of a Throatless Diverging Rotating Detonation Engine, 39th International Symposium on Combustion, 4F10, July 24-29, 2022, Vancouver, Canada.
T. Sato, K. Ishihara, K. Yoneyama, S. Ito, N. Itouyama, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, Experimental Research on Thrust Performance of Rotating Detonation Engine with Liquid Ethanol and Gaseous Oxygen, AIAA Aviation 2022 Forum, AIAA 2022-4143, June 19-July 1, 2022, Chicago & Virtual, USA.
T. Sada, A. Matsuo, E. Shima, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, Numerical Investigation of Rotating Detonation Engine with Injection from the Combustor Side Wall, AIAA Aviation 2022 Forum, AIAA 2022-4108, June 19-July 1, 2022, Chicago & Virtual, USA.
T. Sada, A. Matsuo, E. Shima, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, Three-Dimensional Numerical Investigation on the Effect of Injector Configuration in Rotating Detonation Engine, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 210, June 19-24, 2022, Napoli, Italy.
A. Kawasaki, H. Hasegawa, H. Sun, H. Watanabe, N. Itouyama, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Data-driven Modeling of Reflection Point Distance Relevant to Diffracting Detonation Wave by using Machine Learning, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 246, June 19-24, 2022, Napoli, Italy.
R. Tanaka, A. Matsuo, E. Shima, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, Numerical Investigation of the Effect of Ozone Addition on Detonation in the Two-dimensional RDE Chamber, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 207, June 19-24, 2022, Napoli, Italy.
K. Nakata, K. Ota, S. Ito, 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, Acceleration of Burned gas to Supersonic in a Throatless Rotating Detonation Engine, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 160, June 19-24, 2022, Napoli, Italy.
T. Sato, K. Matsuoka, A. Kawasaki, N. Itouyama, H. Watanabe, J. Kasahara, Experimental Study on Detonation Wave Initiation by Reflected Blast Wave in Laser Ignition, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 179, June 19-24, 2022, Napoli, Italy.
S. Ito, K. Ishihara, K. Yoneyama, K. Goto, N. Itouyama, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of Liquid Propellant Rotating Detonation Combustor, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 170, June 19-24, 2022, Napoli, Italy.
K. Hattori, K. Ota, K. Ishihara, K. Goto, N. Itouyama, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of the Miniaturized Cylindrical Rotating Detonation Engine, 28th The International Colloquium on the Dynamics of Explosions and Reactive Systems (ICDERS), Paper No. 201, June 19-24, 2022, Napoli, Italy.
Kawasaki, A., Matsuyama, K., Matsuoka, Watanabe, H., Itouyama, N., Goto, K., Ishihara, K., Buyakofu., V., Noda, T., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Uchiumi, M., Habu, H., Takeuchi, S., Arakawa, S., Masuda, J., Maehara, K., Nakao, T., Yamada, K.: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: System Design, AIAA SciTech 2022, AIAA-2022-0229, San Diego, CA & Online, January 2022.
Itouyama, N., Matsuyama, K., Matsuoka, Kawasaki, A., Watanabe, H., Goto, K., Ishihara, K., Buyakofu., V., Noda, T., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Uchiumi, M., Habu, H., Takeuchi, S., Arakawa, S., Masuda, J., Maehara, K., Nakao, T., Yamada, K.: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: History from Development to Flight, AIAA SciTech 2022, AIAA-2022-0230, San Diego, CA & Online, January 2022.
Watanabe, H., Matsuyama, K., Matsuoka, Kawasaki, A., Itouyama, N., Goto, K., Ishihara, K., Buyakofu., V., Noda, T., Ito, S., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Uchiumi, M., Habu, H., Takeuchi, S., Arakawa, S., Masuda, J., Maehara, K., Nakao, T., Yamada, K.: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude, AIAA SciTech 2022, AIAA-2022-0231, San Diego, CA & Online, January 2022.
Goto, K., Matsuoka, K., Matsuyama, K., Kawasaki, A., Watanabe, H., Itouyama, N., Ishihara, K., Buyakofu, V., Noda, T., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Uchiumi, M., Habu, H., Takeuchi, S., Arakawa, S., Masuda, J., Maehara, K., Nakao, T., Yamada, K.: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine, AIAA SciTech 2022, AIAA-2022-0232, San Diego, CA & Online, January 2022.
Buyakofu, V., Matsuoka, K., Matsuyama, K., Goto, K., Kawasaki, A., Watanabe, H., Itouyama, N., Ishihara, K., Noda, T., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Uchiumi, M., Habu, H., Takeuchi, S., Arakawa, S., Masuda, J., Maehara, K., Nakao, T., Yamada, K “Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Pulse Detonation Engine”, AIAA Scitech2022, AIAA-2022-0233, San Diego, CA & Online, 2022.
K. Ota, K. Goto, N. Itouyama, H. Watanabe, A. Kawasaki, K. Matsuoka, and J. Kasahara, A. Matsuo, I. Funaki, Study of Cylindrical Rotating Detonation Engine with Propellant Injection Cooling System, AIAA 2021-3650, AIAA Propulsion and Energy, Aug. 9-11, 2021, Virtual Event.
K. Nakata, K. Ota, S. Ito, K. Ishihara, K. Goto, N. Itouyama, H. Watanabe, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study on Truncated Conical Rotating Detonation Engine with Diverging Flows, AIAA 2021-3657, AIAA Propulsion and Energy, Aug. 9-11, 2021, Virtual Event.
S. Sawada, K. Goto, K. Ishihara, A. Kawasaki, K. Matsuoka, and J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of Torque Around the Thrust Axis on a Rotating Detonation Engine, Asian Joint Conference on Propulsion and Power (AJCPP) 2021, 3-5 March 2021, Virtual Conference.
K. Ishihara, K. Yoneyama, S. Ito, H. Watanabe, N. Itouyama, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, and I. Funaki, Study on the Effect of the Difference between Detonation and Constantpressure Combustion on Thrust Characteristics, Asian Joint Conference on Propulsion and Power (AJCPP) 2021, 3-5 March 2021, Virtual Conference.
R. Yokoo, K. Goto, J. Kasahara, V. Athmanathan, J. Braun, G. Paniagua, T. Meyer, A. Kawasaki, K. Matsuoka, A. Matsuo, I. Funaki, Experimental Study of Internal Flow Structures in Cylindrical Rotating Detonation Engines, 38th International Symposium on Combustion, 24-29 January 2021, Adelaide, Australia.
H. Sun, A. Kawasaki, K. Matsuoka, J. Kasahara, A Study on Detonation-Diffraction Reflection Point Distances in H2/O2, C2H2/O2, and C2H4/O2 Systems, 38th International Symposium on Combustion, Adelaide, Australia, 24-29 January 2021.
M. Yamaguchi, K. Matsuoka, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, Investigation of combustion modes and pressure of reflective shuttling detonation combustor, 38th International Symposium on Combustion, 24-29 January 2021, Adelaide, Australia.
H. Watanabe, A. Matsuo, A. Chinnayya, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical Analysis on Behavior of Dilute Water Droplets in Detonation, 38th International Symposium on Combustion, 24-29 January 2021, Adelaide, Australia.
T. Sato, A. Alberti, A. Munafò, M. Panesi, K. Matsuoka, A. Kawasaki and J. Kasahara, Numerical study on early-times laser controlled detonative propulsion, AIAA 2021-0802, AIAA SciTech 2021 Forum, 11–15 and 19–21 January 2021, VIRTUAL EVENT.
K. Goto, K. Ota, A. Kawasaki, H. Watanabe, N. Itouyama, K. Matsuoka, J. Kasahara, A. Matsuo and I. Funaki, Propulsive Performance of Cylindrical Rotating Detonation Engine with Propellant Injection Cooing, AIAA 2021-1029, AIAA SciTech 2021 Forum, 11–15 and 19–21 January 2021, VIRTUAL EVENT.
S. Sawada, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo and I. Funaki, Experimental Measurement of Torque and Force on a Rotating Detonation Engine with Six-Axis Force Sensor, AIAA 2021-0295, AIAA SciTech 2021 Forum, 11–15 and 19–21 January 2021, VIRTUAL EVENT.
J. Kasahara, K. Goto, R. Yokoo, B. Valentin, A. Kawasaki, K. Matsuoka, and K. Matsuyama, Research and Development of Detonation Engine System for the Sounding Rocket Flight Experiment S-520-31, 12th International Colloquium on Pulsed and Continuous Detonations, 19-22 October, 2020, St. Petersburg, Russia.
K. Goto, K. Ota, A. Kawasaki, H. Watanabe, N. Itouyama, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Cylindrical Rotating Detonation Engine Cooling by Means of Propellant Injection, AIAA-2020-3855, AIAA Propulsion and Energy 2020, Aug. 24-28, 2020, Virtual event.
T. Suzuki, A. Matsuo, Y. Daimon, H. Kawashima, A. Kawasaki, K. Matsuoka, and J. Kasahara, Prediction of Pressure Loss in Injector for Rotating Detonation Engines Using Single-element Simulations, AIAA 2020-3879, AIAA Propulsion and Energy 2020, Aug. 24-28, 2020, Virtual event.
R. Yokoo, K. Goto, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Combustion Pressure Distributions and Thrust Performances in Small Cylindrical Rotating Detonation Engines, AIAA-2020-0202, AIAA SciTech Forum, Jan. 6-10, 2020, Orland, Florida, USA.
M. Asahara, J. Kasahara, M. Matsuoka, A. Kawasaki, Pressure and Visualization Measurements on Pulsed Combustor Thrustor, AIAA-2020-0923, AIAA SciTech Forum, Jan. 6-10, 2020, Orland, Florida, USA.
M. Yamaguchi, K. Matsuoka, A. Kawasaki, J. Kasahara, Mode Classification of Combustion and Propulsive Performance of Reflective Shuttling Detonation Combustor, AIAA-2020-1171, AIAA SciTech Forum, Jan. 6-10, 2020, Orland, Florida, USA
T. Sato, K. Matsuoka, A. Kawasaki, J. Kasahara, Experimental Study on Shortening Deflagration-to-Detonation Transition by Nanosecond Laser Ignition, AIAA-2019-3872, AIAA Propulsion and Energy, Aug. 19-22, 2019, Indianapolis, Indiana, USA.
H. Watanabe, A. Matsuo, A. Chinnayya, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical Investigation on Characteristic Lengths for Gaseous Detonation with Dilute Water Spray, AIAA-2019-4132, AIAA Propulsion and Energy, Aug. 19-22, 2019, Indianapolis, Indiana, USA.
A. Kawasaki, R. Yokoo, K. Goto, J.H. Kim, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, An Experimental Study of In-Space Rotating Detonation Rocket Engine with Cylindrical Configuration, AIAA-2019-4298, AIAA Propulsion and Energy, Aug. 19-22, 2019, Indianapolis, Indiana, USA.
H. Watanabe, A. Matsuo, A. Chinnayya, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical Investigation on Effect of Dilute Water Spray on Mean Structure for Gaseous Detonation, 196, 27th International Colloquium on the Dynamics of Explosions and Reactive Systems,July 28-August 2, 2019, Beijing, China.
T. Sato, K. Matsuoka, A. Kawasaki, J. Kasahara, Experimental Study on Deflagration-to-Detonation Transition Shortening by Nanosecond Pulsed Laser Ignition, 240, 27th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 28-August 2, 2019, Beijing, China.
S. Shigeoka, A. Matsuo, A. Kawasaki, J. Kasahara, K. Matsuoka, The Numerical Investigation of Hydrogen Detonation Propagating in Semi-Confined Layers, 138, 27th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 28-August 2, 2019, Beijing, China.
K. Goto, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, D. Nakata, R. Yokoo, J. Kim, I. Funaki, M. Uchiumi, Propulsive Performance of Rotating Detonation Engines in CH4/O2 and C2H4/O2 for Flight Experiment, 245, 27th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 28-August 2, 2019, Beijing, China.
R. Yokoo, K. Goto, J. Kim, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Propulsion Performance of Inner-Cylinder-Less Rotating Detonation Engine, SciTech 2019, 57th AIAA Aerospace Science Meeting, AIAA 2019-1500, January 7-11, 2019, San Diego, California, USA.
K. Goto, R. Yokoo, J. Kim, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, Experimental Performance Validation of a Rotating Detonation Engine toward a Flight Demonstration, SciTech 2019, 57th AIAA Aerospace Science Meeting, AIAA 2019-1501, January 7-11, 2019, San Diego, California, USA.
H. Watanabe, A. Matsuo, K. Matsuoka, A. Kawasaki, J. Kasahara, Numerical investigation of the effect of water spray on irregular and regular gaseous detonation, 11th International Colloquium on Pulsed and Continuous Detonations (ICPCD), September 17–21, 2018 in St. Petersburg, Russia.
H. Taki, K. Matsuoka, A. Kawasaki, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, Study on Burned Gas Purge Process with the Detonable Mixture for High-Frequency Pulse Detonation Cycle, 1P160, 37th International Symposium on Combustion, 29 July- 3 Aug, 2018, Dublin, Ireland.
J. Higashi, Y. Sato, J. Kasahara, A. Kawasaki, K. Matsuoka, A. Matsuo, I. Funaki, Experimental Study of a Disk-Shaped Rotating Detonation Combustor with a Low-Loss-Inlet, 1P154, 37th International Symposium on Combustion, 29 July- 3 Aug, 2018, Dublin, Ireland./li>
J. Kasahara, Research and Development of Rotation Detonation Engines for Sounding Rocket Flight Experiments, The 15th International Space Conference of Pacific-basin Societies (ISCOPS), July. 10-13, 2018, McGill Institute for Aerospace Engineering, Montreal, Canada.
K. Goto, J. Nishimura1, J. Higashi1, H. Taki, T. Ukai, Y. Hayamizu, K. Kikuchi, T. Yamada, S. Watanabe, K. Hotta, T. Inakawa, A. Kubota, M. Yamaguchi, T. Daicho, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Preliminary Experiments on Rotating Detonation Rocket Engine for Flight Demonstration Using Sounding Rocket, SciTech 2018, 56th AIAA Aerospace Science Meeting, AIAA 2018-0157, January 8-12, 2018, Kissimmee, Florida, USA.
J. Kasahara, K. Ishihara, J. Nishimura, S. Nakagami, K. Matsuoka, A. Matsuo, I. Funaki, H. Mukae, K. Yasuda, D. Nakata, K. Higashino, Research and Development of Rotating Detonation Engines for the Sounding Rocket Flight Experiment, International Constant Volume and Detonation Combustion Workshop, 13-15 June 2017, Poitiers, France.
H. Watanabe, A. Matsuo, H. Taki, K. Matsuoka, J. Kasahara, Numerical Investigation on the Effect of Fuel Supply in High Frequency Pulse Detonation Operation, International Constant Volume and Detonation Combustion Workshop, 13-15 June 2017, Poitiers, France.
K. Matsuoka, H. Taki, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, Study on High-Frequency Pulse Detonation Operation, International Constant Volume and Detonation Combustion Workshop, 13-15 June 2017, Poitiers, France.
J. Nishimura, K. Ishihara, K. Goto, S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Mukae, K. Yasuda, D. Nakata, K. Higashino, H. Moriai, Performance Evaluation of a Rotating Detonation Engine, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 30-August 4, 2017, Boston USA.
H. Taki, N. Hirota, K. Matsuoka, K. Akira, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, Pulse Detonation Operation at Kilohertz Frequency, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 30-August 4, 2017, Boston USA.
J. Kasahara, A. Kawasaki, Critical Condition for Detonation Diffraction with Stable and Unstable Mixtures, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 30-August 4, 2017, Boston USA.
H. Rhee, C. Ishiyama, J. Higashi, A. Kawasaki, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study on a Rotating Detonation Turbine Engine with an Axial Turbine, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 30-August 4, 2017, Boston USA.
Y. Sato, A. Matsuo, J. Higashi, C. Ishiyama, K. Matsuoka, J. Kasahara, Numerical Investigation on the Behavior of Detonation Waves in Disk-Shaped Rotating Combustor, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 30-August 4, 2017, Boston USA.
Y. Kumazawa, A. Matsuo, S. Nakagami, K. Matsuoka, J. Kasahara, Numerical Investigation on Detonation Behavior in a Disc-Shaped Rotating Detonation Combustor, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 30-August 4, 2017, Boston USA.
N. Ohira, A. Matsuo, J. Kasahara, K. Matsuoka, Numerical Investigation on Characteristics of a Planar Detonation Wave Across Layers of Burned Gas, 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, 994, July 30- Aug.4, 2017, Boston, USA.
H. Taki, K. Takao, N. Hirota, K. Matsuoka, J. Kasahara, H. Watanabe, A. Matsuo, and T. Endo, Investigation of High - Frequency Pulse Detonation Cycle with Fuel Phase Transition, 31st International Symposium on Shock Waves, SBM000364, July 9-14, 2017, Nagoya, Japan.
J. Nishimura, K. Ishihara, K. Goto, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, H. Mukae, K. Yasuda, D. Nakata, K. Higashino and H. Moriai, Experimental Research on a Long Duration Operation of a Rotating Detonation Engine, 31st International Symposium on Shock Waves, SBM000321, July 9-14, 2017, Nagoya, Japan.
K. Ishihara, J. Nishimura, K. Goto, S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Study on a Long-time Operation Towards Rotating Detonation Rocket Engine Flight Demonstration, SciTech 2017, 55th AIAA Aerospace Science Meeting, AIAA 2017-1062, January 8-12, 2017, Grapevine Texas, USA.
H. Watanabe, A. Matsuo, K. Matsuoka, J. Kasahara, Numerical Investigation on Burned Gas Backflow in Liquid Fuel Purge Method, SciTech 2017, 55th AIAA Aerospace Science Meeting, AIAA 2017-1284, January 8-12, 2017, Grapevine Texas, USA.
J. Higashi, S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of the Disc-Shaped Rotating Detonation Turbine Engine, SciTech 2017, 55th AIAA Aerospace Science Meeting, AIAA 2017-1286, January 8-12, 2017, Grapevine Texas, USA.
Y. Kumazawa, J. Fujii, A. Matsuo, S. Nakagami, K. Matsuoka, J. Kasahara, Numerical Investigation of the Effect of Non-Premixed Injection on Rotating Detonation Propagation, 36th International Symposium on Combustion, 4P133, July 31-August 5, 2016, Seoul, Korea.
H. Watanabe, A. Matsuo, K. Muto, K. Matsuoka, J. Kasahara, T. Endo, One-Dimensional Investigation of Purging Process in Liquid Fuel Purge Method, 36th International Symposium on Combustion, 4P141, July 31-August 5, 2016, Seoul, Korea.
K. Goto, Y. Kato, K. Ishihara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of Effects of Injector Configurations on Rotating Detonation Engine Performance, Propulsion and Energy 2016,52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA 2016-5100, July 25-27, 2016, Salt Lake City, Utah, USA.
J. Fujii, Y. Kumazawa, A. Matsuo, S. Nakagami, K. Matsuoka, J. Kasahara, Numerical Simulation towards Investigating the Factor for Velocity Decrease of Detonation Wave in Rotating Detonation Engine Chamber, Propulsion and Energy 2016,52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA 2016-5101, July 25-27, 2016, Salt Lake City, Utah, USA.
Y. Kumazawa, J. Fujii, A. Matsuo, S. Nakagami, K. Matsuoka, J. Kasahara, Numerical Study for Rotating Detonation Propagation in a Two-Parallel-Plane Combustor, Propulsion and Energy 2016,52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA 2016-5102, July 25-27, 2016, Salt Lake City, Utah, USA.
C. Ishiyama, K. Miyazaki, S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Study of Research of Centrifugal-Compressor-Radial-Turbine Type Rotating Detonation Engine, Propulsion and Energy 2016,52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA 2016-5103, July 25-27, 2016, Salt Lake City, Utah, USA.
S. Nakagami, K. Matsuoka, J. Kasahara, Y. Kumazawa, J. Fujii, A. Matsuo, I. Funaki, Structure of Rotating Detonation Waves in a Two-Parallel-Plane Combustor with Orthogonally Mixing Injectors, AJCPP2016-155, Asian Joint Conference on Propulsion and Power, March 16-19, 2016, Sunport Hall Takamatsu, Kagawa, Japan.
K. Ishihara, Y. Kato, K. Goto, K. Matsuoka, J. Kasahara, Y. Sato, A. Matsuo, I. Funaki, Experimental Flow Analysis of the Combustion Channel Flow of a Rotating Detonation Engine, AJCPP2016-157, Asian Joint Conference on Propulsion and Power, March 16-19, 2016, Sunport Hall Takamatsu, Kagawa, Japan.
S. Takagi, K. Hosono, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Experimental Performance Evaluation of 3N-Class Pulse Detonation Thruster using Liquid Purge Method, SciTech 2016, 54th AIAA Aerospace Sciences Meeting, AIAA 2016-0122, January 4-8, 2016, San Diego, California, USA.
K. Muto, K. Matsuoka, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, Development of High-Frequency Pulse Detonation Combustor without Purging Material, SciTech 2016, 54th AIAA Aerospace Sciences Meeting, AIAA 2016-0123, January 4-8, 2016, San Diego, California, USA.
H. Watanabe, A. Matsuo, K. Muto, K. Matsuoka, J. Kasahara, T. Endo, One-Dimensional Numerical Investigation on Purging the Burned Gas by the Evaporation of Water Droplets in Pulse Detonation Combustor, SciTech 2016, 54th AIAA Aerospace Sciences Meeting, AIAA 2016-1401, January 4-8, 2016, San Diego, California, USA.
Y. Kato, K. Ishihara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Study of Combustion Chamber Characteristic Length in Rotating Detonation Engine with Convergent-Divergent Nozzle, SciTech 2016, 54th AIAA Aerospace Sciences Meeting, AIAA 2016-1406, January 4-8, 2016, San Diego, California, USA.
K. Matsuoka, K. Muto, J. Kasahara, H. Watanabe, A. Matsuo, T. Endo, Development of a liquidpurge method for valvelss pulse detonation combustor using liquid fuel and oxidizer, The 25th International Colloquium on the Dynamics of Explosions and Reactive Systems, Leeds, UK, 2-7 August 2, 2015.
T. Hayashi, A. Matsuo, J. Kasahara, The effect of radius of curvature on the detonation propagating to the unconfined Space, The 25th International Colloquium on the Dynamics of Explosions and Reactive Systems, Leeds, UK, 2-7 August 2, 2015.
J. Fujii, A. Matsuo, J. Kasahara, Two-dimensional simulation on detonation wave supported by the cylindrical inner wall injecting premixed gas, The 25th International Colloquium on the Dynamics of Explosions and Reactive Systems, Leeds, UK, 2-7 August 2, 2015.
K. Ishihara, Y. Kato, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Thrust performance evaluation of a rotating detonation engine with a conical plug, The 25th International Colloquium on the Dynamics of Explosions and Reactive Systems, Leeds, UK, 2-7 August 2, 2015.
S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Schlieren-System-Visualization of Combustion Phenomena in a Two-Parallel-Plane Combustor, Propulsion and Energy 2015, 51st AIAA/SAE/ASEE Joint Propulsion Conference, AIAA 2015-4102, July 27-29, 2015, Orland, Florida, USA.
K. Ishihara, Y. Kato, K. Matsuoka, J. Kasahara, A. Matsuo, and I. Funaki, Experimentally Performance Evaluation of a Rotating Detonation Engine with a Conical-shape Nozzle, 2015-a-30, 30th ISTS, July 4-7, 2015, Kobe, Japan.
K. Ishihara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Performance Evaluation of a Rotating Detonation Engine with Conical Shape Tail, SciTech 2015, 53rd AIAA Aerospace Sciences Meeting, AIAA 2015-0630, January 5-9, Kissimmee, Florida, 2015, USA
S. Nakagami, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Visualization of Rotating Detonation Waves in a Plane Combustor with a Cylindrical Wall Injector, SciTech 2015, 53rd AIAA Aerospace Sciences Meeting, AIAA 2015-0877, January 5-9, Kissimmee, Florida, 2015, USA
K. Matsuoka, S. Takagi, J. Kasahara, T. Morozumi, A. Matsuo and I. Funaki, Flight Demonstration of a Rotary-Valved Four-Cylinder Pulse Detonation Rocket Todoroki II, 14th International Space Conference of Pacific-basin Societies (ISCOPS), May. 28 - 30, 2014, Xi'an, China.
K. Matsuoka, T. Morozumi, S. Takagi, J. Kasahara, A. Matsuo and I. Funaki, Flight Demonstration of a Pulse Detonation Rocket System Todoroki II, 65th International Astronautical Congress 2014, Sep. 29 - Oct 3, 2014, Toronto, Canada.
K. Matsuoka, T. Morozumi, S. Takagi, J. Kasahara, A. Matsuo, I. Funaki, Flight Demonstration of a RotarValved Four Cylinder Pulse Detonation Rocket Engine "Todoroki II", 35th International Symposium on Combustion, San Francisco, August 3-8, 2014. USA
S. Takagi, T. Morozumi, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, Study on Pulse Detonation Rocket Engine Using Flight Test Demonstrator "Todoroki II" , AIAA 2014-4033, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, July 28-30, 2014, US.
Y. Kato, K. Gawahara, K. Matsuoka, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, K. Higashino, N. Tanatsugu, Thrust Measurement of Rotating Detonation Engine by Sled Test, AIAA 2014-4034, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, July 28-30, 2014, US.
Y. Yamagishi, H. Sakakita, S. Tsunoda, J. Kasahara, J. Kim, S. Kiyama, Y. Ikehara, H. Yamada, “Study on the electrical characteristics between the atmospheric pressure plasma and the neutral gas flow”, Plasma Conference 2014, Niigata (2014.11.18-21).
Yusuke YAMAGISHI, Hiromasa YAMADA, Hajime SAKAKITA, Syuichiro TSUNODA, J. Kasahara, Jaeho KIM, Susumu KATO, Hirotomo ITAGAKI, Satoru KIYAMA, Masanori FUJIWARA, and Yuzuru IKEHARA, “Flow control of a neutral gas along with an atmospheric pressure plasma flare”, ISPlasma 2015, Nagoya (2015/03/26-31).
T. Morozumi, R. Sakamoto, T. Kashiwazaki, K. Matsuoka, S. Takagi, J. Kasahara, A. Matsuo, I. Funaki, Study on a Rotary-Valved Four-Cylinder Pulse Detonation Rocket: Thrust Measurement by Ground Test, SciTech 2014, 52nd AIAA Aerospace Sciences Meeting, AIAA 2014-1317, January 13-17, 2014, National Harbor, Maryland, USA
K. Matsuoka, S. Takagi, J. Kasahara, T. Morozumi, T. Kashiwazaki, Y. Fujiwara, A. Matsuo, I. Funaki, Study on a Rotary-Valved Four-Cylinder Pulse Detonation Rocket: Six Degree-of-Freedom Flight Measurement, SciTech2014, 52nd AIAA Aerospace Sciences Meeting, AIAA 2014-1319, January 13-17, 2014, National Harbor, Maryland, USA
T. Ashida, and J. Kasahara, Study on Detonation-Engine Momentum-and-Thrust Loss Measurement by Ballistic Pendulum and Laser Displacement Method, SciTech2014, 52nd AIAA Aerospace Sciences Meeting, AIAA 2014-1016, January 13-17, 2014, National Harbor, Maryland, USA
S. Sumiya, S. Maeda, J. Kasahara, A. Matsuo, Reflection Phenomena of Oblique Detonation Wave around Hypersonic Spherical Projectiles on Plane Plate, SciTech2014, 52nd AIAA Aerospace Sciences Meeting, AIAA 2014-1504, January 13-17, 2014, National Harbor, Maryland, USA
K. Gawahara, H. Nakayama, J. Kasahara, S. Tomioka, T. Hiraiwa, Detonation engine development for reaction control systems of a spacecraft, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit and 11th International Energy Conversion Engineering Conference, AIAA-2013-3721, July 15 ・17, 2013, San Jose Convention Center, San Jose, California, USA
S. Maeda, S. Satoshi, J. Kasahara, A. Matsuo, Scale Effect of Spherical Projectiles for Stabilization of Oblique Detonation Waves, The 24th International Colloquium on the Dynamics of Explosions and Reactive Systems, Taipei, Taiwan, July 28-August 2, 2013
Y. Sugiyama, A. Matsuo, H. Nakayama, J. Kasahara, Numerical Investigation of Detonation Behavior Propagating in Two-dimensional Curved Channel, The 24th International Colloquium on the Dynamics of Explosions and Reactive Systems, Taipei, Taiwan, July 28-August 2, 2013
榊田 創,金 載浩,S. Tsunoda,J. Kasahara,山岸 祐介,Turbulent Phenomena Induced by a Plasma Flow under Atmospheric Pressure Regime,International workshop on the interrelationship between plasma experiments in the laboratory and in space (IPELS),P-4,長野,2013/07/02
山岸 祐介,榊田 創,角田秀一郎,笠原次郎,金 載浩,池原 譲,山田 大将,Akiko Kubota,木山 学,Study on Electrostatic Characteristics of the neutral gas flow along the atmospheric pressure plasma jet,8th International Conference on Reactive Plasmas 2014,福岡,2014/02/05
K. Gawahara, H. Nakayama, J. Kasahara, S. Tomioka, T. Hiraiwa, Detonation engine development for reaction control systems of a spacecraft, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit and 11th International Energy Conversion Engineering Conference, AIAA-2013-????, July 15 ・17, 2013, San Jose Convention Center, San Jose, California, USA
S. Maeda, S. Satoshi, J. Kasahara, A. Matsuo, Scale Effect of Spherical Projectiles for Stabilization of Oblique Detonation Waves, The 24th International Colloquium on the Dynamics of Explosions and Reactive Systems, Taipei, July 28-August 2, 2013
Y. Sugiyama, A. Matsuo, H. Nakayama, J. Kasahara, Numerical Investigation of Detonation Behavior Propagating in Two-dimensional Curved Channel, The 24th International Colloquium on the Dynamics of Explosions and Reactive Systems, Taipei, July 28-August 2, 2013
T. Morozumi, K. Matsuoka, R. Sakamoto, Y. Fujiwara, J. Kasahara, A. Matsuo, I. Funaki, Study on a Four-Cylinder Pulse Detonation Rocket Engine with a Coaxial High Frequency Rotary Valve, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2013-0279, January 7-10, 2013, Grapevine, Texas, USA
T. Uruno, S. Maeda, J. Kasahara, A. Matsuo, Study on Detonation Wave Attenuation through Narrow Tube for Application to Explosion Safety and Detonation Engines, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2013-0885, January 7-10, 2013, Grapevine, Texas, USA
J. Kasahara, K. Matsuoka, S. Sakamoto, K. B. Ikeguchi, T. Sakumi, T. Morozumi, A. Matsuo, I. Funaki, Multitube-Rotary-Valved Pulse Detoanation Rocket Engine for Flight Test, International Workshop on Detonation for Propulsion 2012, September 3-5, 2012, Tsukuba, Japan
H. Nakayama, J. Kasahara, A. Matsuo, I. Funaki, Propagation of Self-sustaining Curved Detonation Waves in Annular Channels with a Rectangular Cross-section, International Workshop on Detonation for Propulsion 2012, September 3-5, 2012, Tsukuba, Japan
J. Kasahara, K. Matsuoka, R. Sakamoto, K. Ikeguchi, T. Sakumi, T. Morozumi, A. Matsuo, I. Funaki, Thrust Measurement of a Four-Cylinder Pulse Detonation Rocket Engine with a Coaxial High Frequency Rotary Valve,8th International Colloquium on Pulsed and Continuous Detonations, June 10-16, 2012, Budva, Montenegro
R. Sakamoto, K. Matsuoka, K. Ikeguchi, T. Sakumi, T. Morozumi, J. Kasahara, A. Matsuo, I. Funaki, Thrust Measurement of a Multi-Cylinder Pulse Detonation Rocket Engine with a Coaxial High Frequency Rotary Valve, Asian Joint Conference on Propulsion and Power, AJCPP2012-080, March 3, 2012, Xi'an, China
H. Nakayama, T. Moriya, J. Kasahara, A. Matsuo,and I. Funaki, Front Shock Behavior of Stable Detonation Waves Propagating Through Rectangular Cross-section Curved Channels, AIAA 2012-0618, 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 9-12 January 2012, Nashville, Tennessee, USA
K. Matsuoka, M. Esumi, K. Ikeguchi, J. Kasahara, A. Matsuo, I. Funaki, Thrust Measurement and Visualization Experiment of a Multi-Cycle Single-Tube Pulse Detonation Rocket Engine with a Coaxial Rotary Valve, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2011-5789, 31 July-3 August, 2011, San Diego, California, USA
S. Maeda, J. Kasahara, A. Matsuo, Visualization of the Initiation and Stabilization Process of an Oblique Detonation Wave Around a Projectile, 23rd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.116, July 24-29, 2011, Irvine, USA.
H. Yamashita, J. Kasahara, A. Matsuo, Visualization Study of Detonation Initiations Behind Reflected Shock Waves Using a High Speed Video Camera, 23rd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.199, July 24-29, 2011, Irvine, USA.
H. Nakayama, T. Moriya, J. Kasahara, A. Matsuo, Y. Sasamoto and I. Funaki, Study on Detonation Waves Propagating through Curved Channels, 23rd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.193, July 24-29, 2011, Irvine, USA.
J.-Y. Choi, S. Maeda, J. Kasahara, A. Matsuo, Drag Coefficients of Hypervelocity Spherical Projectile Initiation Oblique Detonation Wave, 23rd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.282, July 24-29, 2011, Irvine, USA.
S. Maeda, R. Inada, J. Kasahara, A. Matsuo, I. Funaki, The Stabilized Oblique Detonation Wave and Unsteady Wave Structure Around Hyper-Velocity Spherical Projectile, AIAA 2011-0505, 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 4-7 January 2011, Orlando, Florida, USA
S. Takeuchi, N. Doi, J. Kasahara, A. Matsuo, Effect of DDT Process on Impulse of Diaphragm-less Pulse Detonation Tube, 8th Asia-Pacific Conference on Combustion, Paper No. 79, 10-13 December, 2010, Hyderabad, India
Y. Nagura, S. Maeda, Y. Kudo, J. Kasahara, A. Matsuo, Detonation Wave Diffraction in the Vicinity of Corners, 8th International Symposium on Hazards, Prevention, and Mitigation of Industrial Explosions, Paper No. ISH-108, 5-9 September 2010, Yokohama, Japan
Y. Sasamoto, A. Matsuo, J. Kasahara, Numerical analysis of detonation waves structure in bend tube, 8th International Symposium on Hazards, Prevention, and Mitigation of Industrial Explosions, Paper No. ISH-109, 5-9 September 2010, Yokohama, Japan
Y. Nagura, Y. Kudo, J. Kasahara, A. Matsuo, Multi-Frame Visualization Analysis of Two-Dimensional Detonation Wave Diffraction and Re-initiation (Work-in Progress Poster), 33rd International Symposium on Combustion, 1-6 August 2010, Beijing, China
K. Matsuoka, M. Esumi, J. Yageta, T. Nakamichi, J. Kasahara, S. Ogawa, T. Yajima, T. Kojima, Study on Valve Systems for Pulse Detonation Engines, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2010-6672, 25-28 July 2010, Nashville, Tennessee, USA
S. Takeuchi, N. Doi, J. Kasahara, M. Murayama, A. Matsuo, Net Impulse Measurements of Pulse Detonation Tube by Using Fuel-Air Mixture, AIAA 2010-148, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4 - 7 January 2010, Orlando, Florida, USA
K. Matsuoka, J. Yageta, T. Nakamichi, J. Kasahara, T. Yajima, T. Kojima, Study on an Inflow-Drive Valve System for Pulse Detonation Engines, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2009-5313, 2-5 August 2009, Denver, Colorado, USA
K. Kawane, S. Shimada, J. Kasahara, A. Matsuo, The Influence of Heat-Transfer and Friction on the Impulse of a Single-Cycle Pulse Detonation Tube, 22nd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.163, July 27-31 2009, Minsk, Belarus.
A. Uemichi, S. Kato, J. Kasahara, A. Matsuo, Steadiness of Oblique Detonation Waves around Spherical Projectiles, 22nd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.152, July 27-31 2009, Minsk, Belarus.
S. Kato, S. Hashimoto, A. Uemichi, J. Kasahara, A. Matsuo, Study on Propagation Characteristics of Shock Waves Driven by Gaseous Detonation Waves, 22nd International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper No.151, July 27-31 2009, Minsk, Belarus.
A. Tsukui, K. Matsumoto, J. Kasahara, T. Kojima, Research on Interaction Between an Intermittent Flow and a PDE Turbine, 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, AIAA 2009-295, 5-8 January 2009, Orland, Florida, USA
K. Matsuoka, J. Yageta, H. Yamaguchi, J. Kasahara, T. Yajima, T. Kojima, Study on an Autonomous-Drive Valve System of Pulse Detonation Engines, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2008-4881, 21-23 July 2008, Hartford Connecticut, USA
K. Matsuoka, H. Yamaguchi, T. Nemoto, J. Yageta, J. Kasahara, T. Yajima, T. Kojima, Experimental Research of Autonomous Driving Valve for Pulse Detonation Rocket Engine, Asian Joint Conference on Propulsion and Power, Korea, March 2008, Gyeongju
Y. Takashima, J. Kasahara, J. E. Shepherd, and I. Funaki, Impulse Generation by a Shock Tube in a Vacuum, 46th AIAA Aerospace Science Meeting and Exhibit, AIAA 2008-987, USA, January 2008, Reno
J. Kasahara, A. Hasegawa, T. Nemoto, H. yamaguchi, T. Yajima, F. Yamamoto, H. Tanaka, and T. Kojima, Horizontal Gliding Test of a Pulse Detonation Rocket System, 7th International Symposium on Special Topics in Chemical Propulsion, September 2007, Kyoto
J. Kasahara, A. Hasegawa, T. Nemoto, H. yamaguchi, T. Yajima, Thrust Demonstration of a Pulse Detonation Rocket "TODOROKI", 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2007-5007, USA, 2007, Cincinnati
T. Fujino, Y. Matsumoto, J. Kasahara, and M. Ishikawa, Numerical Studies of Magnetohydrodynamic Flow Control Considering Real Wall Electrical Conductivity, AIAA-2006-2892, 37th-AIAA Plasmadynamics and Lasers, 2006
T. Kojima, H. Kobayashi, J. Kasahara, Experimental Study on Thrust Increase of Pulse Detonation Engine By High Supply Pressure, Asian Joint Conference on Propulsion and Power 2006, Beijing
T. Kojima, H. Kobayashi, N. Tsuboi, J. Kasahara, Analytical and Experimental Study on PDE with Exit Valves for Thrust Augment, Fifth International Colloquium on Pulsed and Continuous Detonations , July 2006, Moscow
J. Kasahara, M. Hirano, A. Matsuo, S. Sato, T. Endo, Flight Experiment Regarding Ethylene-Oxygen Single-Tube Pulse Detonation Rockets, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2004-3918, USA, 2004, Fort Lauderdale
J. Kasahara, M. Hirano, A. Matsuo, S. Sato, T. Endo, Flight Experiment Regarding Single-Tube Pulse Detonation Rockets, International Colloquium on Application of Detonation for Propulsion, 2004, St. Petersburg, Russia (to be published 2006 in a book)
T. Endo, T. Yatsuhusa, S. Taki, J. Kasahara, A. Matsuo, K. Inaba, S. Sato, Analytical Estimation of the Propulsive Performance of Pulse Detonation Engines, Asian Joint Conference on Propulsion and Power, CD-ROM, March 2004
M. Hirano, J. Kasahara, A. Matsuo, T. Endo, M. Murakami, Thrust-Performance Test of Ethylene-Oxygen Single-Tube Pulse Detonation Rocket, Asian Joint Conference on Propulsion and Power, CD-ROM, March 2004
T. Endo, T. Yatsuhusa, S. Taki, J. Kasahara, A. Matsuo, S. Sato, Homogeneous-Dilution Model of Partially-Fueled Pulse Detonation Engines, AIAA 2004-0214, January 2004, Reno
S. Sato, A. Matsuo, J. Kasahara, T. Endo, Numerical Investigation of the PDRE Performance with Detailed Chemistry, AIAA 2004-0464, January 2004, Reno
J. Kasahara, Y. Tanahashi, M. Hirano, T. Numata, A. Matsuo, T. Endo, Experimental Investigation of Momentum and Heat Transfer in Pulse Detonation Rockets, 42st AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2004-0869, January 2004, Reno
T. Endo, J. Kasahara, Y. Tanahashi, T. Numata, A. Matsuo, S. Sato, T. Fujiwara, Pressure History at the Thrust Wall of a Simplified Pulse Detonation Engine, 19th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 2003, Hakone
S. Sato, A. Matsuo, J. Kasahara, T. Endo, Performance Analysis of the Multiple Tube Pulse Detonation Rocket Engine, 19th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 2003, Hakone
J. Kasahara, Y. Tanahashi, T. Numata, A. Matsuo, T. Endo, Experimental Studies on L/D ratio and Heat Transfer in Pulse Detonation Engines, 19th International Colloquium on the Dynamics of Explosions and Reactive Systems, July 2003, Hakone
J. Kasahara, K. Takazawa, T. Arai, A. Matsuo Experimental Study of Impulse and Heat Transfer on Pulse Detonation Engines, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2002-4071, 2002, Indianapolis, USA
T. Arai, F. Sakima, F. He and, J. Kasahara, Interaction between an Underexpanded Circular Jet Injected Normally into a Supersonic Cross Flow and Boundary Layer, 23rd International Symposium on Space Technology and Science, May 26-June 2, 2002, Matsue, Japan
J. Kasahara, T. Arai, A. Matsuo, N. Akai, K. Takazawa, Critical Condition for Stabilized Chapman-Jouguet Oblique Detonation Waves Around Hypersonic Bodies, 18th International Colloquium on the Dynamics of Explosions and Reactive Systems, 2001年, Paper No.198, Seattle, USA
T. Arai, J. Kasahara, F. Sakima, J. Miura, T. Arai, H. Nagata, Hydrogen Concentration Measurements of Supersonic Hydrogen-Air Shear, Layer Using Catalytic Reaction, AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2001-1773, 2001, Kyoto, Japan
J. Kasahara, T. Arai, A. Matsuo, N. Akai, and K. Takazawa, Experimental Investigations of Steady-State Oblique Detonation Waves Generated Around Hypersonic Projectiles, AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2001-1800, 2001, Kyoto, Japan
T. Arai, J. Kasahara, K. Mizobata, H. Sugiyama, Y. Hanaoka, H. Hoya, Y. Nishi, An Approach for Teaching Aircraft Propulsion Systems Using a Micro Turbojet Engine for Undergraduate Laboratory Course Students in Japanese University, The 8th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-8), 2000, Honolulu, USA
J. Kasahara, T. Arai, T. Endo, T. Fujiwara, Experimental Study of Steady Oblique Detonation Waves Around a Ballistic-Range Projectile, 22nd International Symposium on Space Technology and Science, 2000, pp.1015-1021, Morioka, Japan
J. E. Leblanc, K. Sugiyama, J. Kasahara, T. Fujiwara, Numerical Simulation of Oblique Detonation Experiments at a Ballistic Range, Proceedings of the 22nd International Symposium on Shock Waves, 1999, pp.263-268, London, UK
J. Kasahara, T. Endo, K. Nishide, D. Yahata, N. Yoshikawa, T. Fujiwara Experimental Study on Oxyhydrogen Oblique Detonation Around Hypersonic Projectiles, Proceedings of the 22nd International Symposium on Shock Waves, 1999, pp.303-308, London, UK
J. Kasahara, A. Takeishi, H. Kuroda, M. Horiba, K. Matsukawa, J. E. Leblanc, T. Endo, and T. Fujiwara,Experimental Observation of Oblique Detonation Waves Around Hypersonic Free Projectiles, Ram Accelerators (Proceedings of the Third International Workshop on RAM Accelerators (RAMAC III), 1997.7), eds. K. Takayama and A. Sasoh, Springer Verlag, 1998, pp.263-270, Heidelberg
Endo, J. Kasahara, A. Takeishi, and T. Fujiwara, Experiments on Oblique Detonation Waves Around Hypersonic Cone-Nosed Projectiles, 16th International Colloquium on the Dynamics of Explosions and Reactive Systems, 1997, pp.473-476, Cracow, Poland
T. Endo, J. E. Leblanc, J. Kasahara, and T. Fujiwara, Fundamental Studies of Hypersonic Combustion Waves for Ram Accelerators, The Second International Workshop on RAM Accelerators (RAMAC II), 1995, Seattle, USA
T. Horii, J. Kasahara, T. Endo, and T. Fujiwara, Multi-Frame Observation of Hypersonic Shock-Induced Combustion Wave RAN95, 1995, Nagoya
S. Yano, K. Komurasaki, J. Kasahara, H. Takaoka, and T. Fujiwara, and A. Saito, Radiative Heat Transfer to a Hypersonic Projectile in Ballistic Range Experiments, The 19th International Symposium on Space Technology and Science, 1994, pp.405-410, Yokohama, Japan
Commentary artices, Review articles, Research reports 解説記事・総説・研究報告書
Blandel Mathieu, 松尾亜紀子, 川崎央, 笠原次郎,The reflection point distance of detonation based on two-dimensional simulations,1D08, 第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム, 2021年6月30日-7月2日, オンライン.
25th International Colloquium on the Dynamics of Explosions and Reactive Systems, 特別セッション“Detonation Application in Propulsion”オーガナイザー,Leeds, UK, 2015.
日本燃焼学会デトネーションエンジン研究委員会,幹事(2012.9-2014.8)
筑波大学非常勤講師(2013.5~2014.3)担当科目 圧縮性流れの力学(大学院)
International Workshop on Detonation for Propulsion 2013(ONRスポンサー), オーガナイザー(2013年)
2012 International Workshop on Detonation for Propulsion (USAF, ONR, 日本燃焼学会スポンサー), オーガナイザー(2012年)
2011 International Workshop on Detonation for Propulsion (USAF, ONR, Pusan National Universityスポンサー), オーガナイザー(2011年)
「デトネーションの熱流体力学1基礎編」編集委員会,編集幹事(2010-2011年)
28th International Symposium on Space Technology and Science,開催地委員会, 幹事(2010-2011年)
27th International Symposium on Space Technology and Science,開催地委員会委員(2009年)
27th International Symposium on Space Technology and Science,プログラム小委員会(化学推進)副委員長(2009年)
27th International Symposium on Space Technology and Science,運営委員会委員(2009年)
第14回動力エネルギー技術シンポジウム現地実行委員会委員(2009年)
26th International Symposium on Space Technology and Science, プログラム小委員会(化学推進)副委員長(2008年),The ISTS Special Issue of Transaction of JSASS Aerospace Technology Japan, Editor(2009年)