A.【査読付き学術誌】研究業績

----------------------------2020年度------------------------------------

1. 橋本啓吾, 向江洋人, 湊亮二郎, 中田大将, 内海政春,
   小型超音速機用エンジンの定常軸振動解析による危険速度通過時の軸振動評価,
   ターボ機械, 第48巻第4号, pp.208-215, 2020年4月．
2. Ryoji Imai, Kazuaki Nishida, Osamu Kawanami, Yutaka Umemura and Takehiro Himeno，
   Ground based experiment and numerical calculation on thermodynamic vent system in propellant tank for future cryogenic propulsion,
   Cryogenics, Vol.109, Article 103095, pp1-9, 2020, https://doi.org/10.1016/j.cryogenics.2020.103095, IF: 1.336 Q3
3. 上村典道, 迫悠冬, 堀口祐憲, 内海政春,
   小型軌道投入ロケット用インデューサの設計クライテリアと設計検証事例,
   ターボ機械, 第48巻第10号, pp.605-615, 2020年10月．
4. 今井良二，
   アルミニウム，水高圧水素製造反応の宇宙推進システムへの適用,
   油空圧技術, Vol.59, No.9, p.7-11, 2020年9月．
5. Koki Arimatsu, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi and Masaharu Uchiumii,
   On the Pressure Loss Characteristics of Liquid Oxygen Considering a Heat Input,
   Transaction of JSASS, Aerospace Technology Japan, Vol.19, No.2, pp.217-223, Mar., 2021,
   DOI: 10.2322/tastj.19.217
6. Kazuki Yasuda, Daisuke Nakata, Masaharu Uchiumi, Kugo Okada and Ryoji Imai,
   Fundamental Study on Injector Flow Characteristics of Self-Pressurizing Fluid for Small Rocket Engines,
   Journal of Fluid Engineering, Volume 143, Issue 2, February 2021, p.p.021307
7. Kazuaki Nishida, Ryoji Imai, Osamu Kawanami, Yutaka Umemura and Takehiro Himeno，
   Ground-Based Experiment on Reducing Boil-Off Gas by Jet Mixing for Future Cryogenic PropulsionSystem,
   Int. J. Microgravity Sci. Appl.，Vol.38, No.1, 2021, https://doi.org/10.15011/jasma.38.1.380102.
8. Koichi Inoue, Haruhiko Ohta, Yuuki Toyoshima, Hitoshi Asano, Osamu Kawanami, Ryoji Imai, Koichi Suzuki, Yasuhisa Shinmoto, Satoshi Matsumoto,
   Heat Loss Analysis of Flow Boiling Experiments onboard International Space Station with unclear thermal environmental conditions(1st Report: Subcooled liquid flow conditions at test section inlet).，
   Microgravity 14Science and Technology, Vol.33, No.3, Article 28,2021,
   https://doi.org/10.1007/s12217-021-09869-5. IF: 1.845
9. Keisuke Goto, Yuichi Kato, Kazuki Ishihara, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Kazuyuki Higashino and Nobuhiro Tanatsugu,
   Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled Test,
   Journal of Propulsion and Power, Published Online:1 Dec 2020, https://doi.org/10.2514/1.B38037, Vol.37, No.3, 2021, pp.419-425, doi:doi/abs/10.2514/1.B38037