研究業績

査読付き学術誌

-------------------------2008年度-------------------------------------
［1］ 棚次亘弘, 室蘭工業大学における航空宇宙分野の実践教育, 工学教育, Vol.56, No.5, （2008）,　pp.79-83,20.
［2］ 吹場活佳, 井上翔, 佐藤哲也, 大久保英敏, 予冷ターボジェットエンジンにおけるジェット噴射を用いた熱交換器の除霜, 日本航空宇宙学会論文集, Vol.56, No.657, （2008）, pp. 464-470.
[3] 湊亮二郎, 溝端一秀, 桑田耕明, 吸込み式超音速風洞におけるスターティングロードの計測と供試体の挙動, 日本航空宇宙学会論文集, Vol.56, No.659, （2008）, pp.580-589.
［4］ 渡邉真也, 湊亮二郎, 多数非劣解集合からの設計支援手法の開発－ジェットエンジン最適化を通して, 人工知能学会論文誌, Vol.24, No.1, （2009）.
--------------------------2009年度-------------------------------------
［5］ Fukiba, k., Inoue, S., Ohkubo, H., and Sato, T., “A New Defrosting Method Using Jet Impingement for Precooled Turbojet Engines,” AIAA Journal of Thermophysics and Heat Transfer, Vol.23, No.3, 2009, pp. 533-542.
［6］ 東野和幸, 杉岡正敏, 小林隆夫, 湊亮二郎, 丸祐介, 笹山容資, 大塚雅也（室蘭工大）, 牧野隆（ＩＨＩ）, 坂口裕之（ＩＨＩエアロスペース）, ＬＮＧロケットエンジンのコーキング特性に関する基盤研究, 日本航空宇宙学会論文集, Vol.57, No.664,　（2009）, pp.210-216.
［7］ Nishizawa, A., Tokugawa,N., and Takagi, S., “Critical Reynolds number off the attachment-line boundary layer on a yawed cylinder,” Fluid Dynamics Research, Vol. 41, No.3, 2009, pp.385-392.
［8］ Atobe, T., Tuinstra, M., and Takagi, S., “A study on airfoil tonal noise generation in resonant environments,”Transactions of Japan Society of Aeronautical and Space Sciences, Vol.52, No.176, 2009, pp.74-80.
--------------------------2010年度------------------------------------
［9］ Takagi, S., and Konishi, Y., “ Suppression of Trailing-Edge Noise Emitted by Two-　Dimensional Airfoils,”Transactions of Japan Society of Aeronautical and Space Sciences, Vol.53, No.179,2010, pp.19-23.　
［10］ Minato. R, Mizobata, K., and Kuwada, K., “Experimental Measurements of Starting Loads and Model behaviors in the Indraft Supersonic Wind Tunneld, “ Transaction of the Japan Society for Aeronautics and Space Science,　Vol.53, No.179, 2010, pp.54-62.
［11］ 東野和幸, 杉岡正敏, 小林隆夫, 境昌宏, 湊亮二郎, LNGロケットエンジンのサルファアタック及びコーキングに関する基礎的研究, 日本航空宇宙学会論文集, Vol.57, No.670, （2010）, pp.445-452.
［12］ 東野和幸, 杉岡正敏, 小林隆夫, 湊亮二郎, 大屋俊輔, 笹山容資, グラファイトコーティングを利用した再生冷却型LNGロケットエンジンのコーキング抑制, 日本航空宇宙学会論文集, Vol.58, No.676, （2010）, pp.138-145.
［13］ Takagi, S, and Konishi, Y., “On the Frequency Selection Mechanism of Airfoil　Trailing-Edge Noise,”Journal of Aircraft, Vol. 47, No.4, 2010, pp.1111-1116.
［14］ 東野和幸, 駒崎慎一, 木元健一, 坂口裕之, 石橋利幸, ロケット燃焼室におけるニッケル電鋳特性向上に関する基礎研究, 日本航空宇宙学会論文集, Vol.58, No.676,（2010）, pp.146-151.
［15］ 吹場活佳, 坪井伸幸, 小林弘明, ノーズコーンをもつ超音速機の壁面圧力を用いた機体姿勢およびマッハ数計測に関する数値解析, 日本航空宇宙学会論文集, Vol.58, No.676, (2010), pp. 130-137.
［16］ 神田康晴, 上道芳夫, 杉岡正敏, 廃アルミニウムからの水素製造, 化学工学, Vol.74, No.2, (2010), pp.60-62.
［17］ Kanda,Y., Temma, C., K. Nakata, T., Kobayashi, Sugioka, M., Uemichi, Y.,“Pｒeparation and performance of noble metal phosphides on silica as new hydrodesulfurization catalysts”, Applied Catalysis A,”　General, Vol.386, 2010, pp.171-178.
［18］ Sato, T., Taguchi, H., Kobayashi, H., Kojima, T., Fukiba, K., Masaki, D., Okai, K., Fujita, K., Hongo, M., Sawai, S., “Development study of a precooled turbojet engine,” Acta Astronautica, Vol.66, Issue 7-8s, 2010, pp. 1169-1176.
[19] Akira Iwakawa, Daisuke Nakata, and Hitoshi Kuninaka, “Experimental Study of a Two-Dimensional Applied Field Magnetoplasmadynamic Thruster,” Aerospace Technology Japan, Vol. 8 (2010) pp.Pb_13-Pb_17, 2010．
［20］ Kasaba, Y., Kumamoto, A., Ishisaka, K, Kojima, H., Higuchi, k., Watanabe, A., and Watanabe, K., “Development of stiff and extensible electromagnetic sensors for space missions,” Advances in Geosciences, Solar & Terrestrial Science, Vol.21, 2010, pp.447-459.
[21] 神田康晴, 小林隆夫, 上道芳夫, 杉岡正敏, 廃アルミニウムによる新規水素製造法の開発―アルミニウム廃材を用いた水素製造法のスケールアップについてー, 配管技術, Vol.53, No.1, (2011), pp.7-11.
---------------------------2011年度------------------------------------
［22］ Nakata, D., Toki, K., Funaki, I., Kuninaka, H., “Performance of ThO2-W, Y2O3-W and La2O3-W cathodes in Quasi-Steady Magnetoplasmadynamic Thrusters,” Journal of Propulsion and Power, Vol. 27, No. 4, 2011, pp. 912-915.
［23］ Asai, M., Inasawa, A., Konishi, Y., Hoshino, S. and Takagi, S., “Experimental investigation of the instability of wakes of axisymmetric streamline body,”Journal of Fluid Mechanics, Vol. 675 , 2011, pp. 574-595.
［24］ 笹山容資, 境昌宏, 小林隆夫, 杉岡正敏, 東野和幸, 東伸幸, 青木賢司, 小林完, 沖田耕一, “LNGロケットエンジンにおけるサルファアタック防止に関する研究　-特に金メッキの特性評価-”，日本航空宇宙学会論文集，Vol.59, No.688, （201１），pp.138-145.
［25］ Kanda, Y., Kondo, S., Ooya, S., Kobayashi, T., Uemichi, Y., Higashino, k., and Sugioka, M.,“Green Hydrogen Production by Mechanical Mixing of Aluminum with Water”, Journal of Chemical Engineering of Japan, Vol.44, No.10, 2011, ｐｐ803-808.
［26］ Ikeda,T., Atobe, T., and Takagi, S., “Direct simulations of trailing-edge noise generation from two-dimensional airfoils at low-Reynolds numbers,” Journal of Sound and Vibration, Vol.331, 2011, pp. 556–574.
［27］ Ohira, M., Umaba, T., Kitazawa, S., Ban, H., Ueba, M., “Experimental Characterization of Microwave Radio Propagation in ICT Equipment for Wireless Harness Communications,” IEEE Transactions on Antennas and Propagation, Vol.50, No.12, 2011, pp.4757-4765.
----------------------------2012年度------------------------------------
［28］ 東野和幸, 杉岡正敏, 棚次亘弘, 湊亮二郎, 笹山容資, 磯田浩志, 熱分解吸熱反応燃料の吸熱量の測定と評価, 日本航空宇宙学会論文集，Vol.60, No.3,（2012），pp.115-120.
［29］ 寺島修, 大西一弘, 酒井康彦, 長田孝二, 髙木正平, 定温度型熱線流速計の周波数応答特性を向上させる試み, 日本機械学会論文集（B編）, Vol.78, No.788, (2012-4), pp.862-866.
［30］ Nakata, D., Kozu, A Yajima, S., Kenji Nishine, Higashino, K., and Tanatsugu, N., “Predicted and Experimented Acceleration Profile of the Rocket Sled,” Aerospace Technology Japan, Vol. 10, No. ists28,　2012, pp. Ta_1-Ta_5.
［31］ Itoh, N., Takagi, S., and Ikeda T., “Instability and frequency selection of the wake behind a flat plate,”Transactions of the Japan Society for Aeronautics and Space Sciences, Vol.55, No.6, 2012, pp356-363.
［32］ Ogi,Y., Higuchi, K., and Ishimura, k.,“Effect of Attachment Errors of Flexible Appendages on the Spin Axis of a Rigid Body,“Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.10, No.28, 2012, pp.Pc_7-Pc_12.
［33］ Ishimura, K., Kii, T., Komatsu, K., Goto, K., Higuchi, K., Matsumoto, k., Iikura, S., Yoshihara, M., Tsuchiya, M.,“Shape Prediction of Large Deployable Antenna Structure on Orbit,” TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, Vol.10, No.28, 2012, pp.Pc_35-Pc_40.
［34］ Kawamura, H., Iwasa, T., Unemitsu, K., Sugiyama,R., Kishimoto, N., Higuchi,K., Fujigagi, M., and Shiokawa, T.,“Visualization on Formation Process of Wrinkling Phenomena on Thin Membranes Using Grating Projection Method and Investigation on Their Nonlinear Mechanical Properties,” TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, Vol.10, No.28,2012, pp.Pc_91-Pc_97.
［35］ 岩佐貴史，采光啓太，杉山遼，岸本直子，樋口健，藤垣元治，塩川貴之, 格子投影法によるポリイミドフィルムの表面形状計測，航空宇宙技術，Vol.11, (2012) pp.69-78.
----------------------------2013年度------------------------------------
［36］ 髙木正平, 山谷直広, 伊藤信毅, 人工音響ループによる二次元噴流不安定波周波数の制御, 日本航空宇宙学会論文集, Vol.6１, No.3, (2013), pp.57-63．
［37］ 石川温士, 今井良二, 田中貴博, SF6-水を用いた水平管群まわりの気液二相流計測, 高温高圧のPWR/SG二次冷却水側の気液二相流を常圧で模擬, 配管技術, Vol.56, No.1, 2014, pp.28-34.
［38］ Koyanagi, J., Watanabe, A., Kawabata, N., Ozaki, T., Higuchi, K., Ishimura, K., and Kasaba, Y., “Long-term durability of tri-axial woven CFRP tube structure extended along the spin axis of spinning platforms for the SCOPE mission,” Advanced Composite Materials, Vol.23, No.2, 2014., pp.115–128.
----------------------------2014年度------------------------------------
[39] Ken HIGUCHI, Yasuyuki MIYAZAKI, Kosei ISHIMURA, Hiroshi FURUYA, Hiroaki TSUNODA, Kei SENDA, Akihito WATANABE, Nobuyoshi KAWABATA, Takeshi KURATOMI, and SIMPLE Project Team, "Initial Operation and Deployment Experiment of Inflatable Extension Mast in SIMPLE on JEM Exposure Platform in ISS," Trans. JSASS Aerospace Tech. Japan, Vol.12, No.ists29, pp.Pc_1-Pc_7, (2014.4).
［40] Daisuke Nakata, Kenji Nishine, Kaoru Tateoke, Kazuyuki Higashino, Nobuhiro Tanatsugu, “Aerodynamic Measurement on the High Speed Test Track,” , Transactions of the Japan Society for Aeronautics and Space Sciences Aerospace Technology Japan, , Vol.12, No.ists29, pp.　Tg　5-Tg　10, 2014．
［41］ Kazuyuki　Higashino，Masatoshi Sugioka, Shuntaro Izumi, Toshiyuki　Terada, Noboyuki　Azuma，Teiu Kobayashi, “Study on Material Compatibility for Bioethanol Fueled Rocket Engine,” Aerospace Technology Japan, Vol.12, No.ists29, pp.　Pa　41-Pa　46, 2014..
［42］ Kazuhide MIZOBATA, Ryojiro MINATO, Ken HIGUCHI, Masazumi UEBA, Syohei TAKAGI, Daisuke NAKATA, Kazuyuki HIGASHINO, and Nobuhiro TANATSUGU, “Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed for Future Space Transportation Research,” ISTS Special Issue: Selected papers from the 29th International Symposium on Space Technology and Science, Transactions of JSASS, Aerospace Technology Japan, , Vol.12, No.ists29, pp.　Po 3 1-Po3 10, 2014.
[43] 塚野　徹、棚次亘弘、杉岡正敏、東野和幸「 白金触媒を用いた熱分解吸熱性燃料の吸熱量の測定と評価」．日本航空宇宙学会論文.第62巻5号、pp.149-156,（2014）.
[44] 髙木正平、上村卓也、平田裕、高田晃輔「超音速流特性に及ぼす湿度効果について」、. 日本航空宇宙学会論文集．第62巻、４号、pp.136-142, (2014)．
[45] Daisuke Nakata, Kiyoshi Kinefuchi，Satoshi Hosoda, Masahiro Kinoshita and Hitoshi Kuninaka “Technical Challengers for Advanced Arcjets,” , Transactions of the Japan Society for Aeronautics and Space Sciences Aerospace Technology Japan,　 Vol.12, No.ists29, pp.　To_1_1-To_1_5, Nov. 2014
[46]髙木正平、「Kuttaの条件を満たした翼周りの流線の可視化　–電界場の等電位線とポテンシャル流の流線とのアナロジを利用して-」、.可視化情報学会論文集．第34巻、9号、pp29-34, (2014)．
[47] Takagi, S., Yamaya, N. and Itoh, N.: Frequency control of unstable disturbances in two-dimensional jet by artificial acoustic loop, Transactions of the Japan Society for Aeronautics and Space Sciences. Vol.57, No.5, 2014, pp.255-262.
[48] Nobuhisa Katsumata, Kaimori Masaaki, Masanobu Yamasaki, Ken Higuchi, Michihiro Natori, Hiroshi Yamakawa: Deployment Characteristics of Braid Coated Bi-Convex Tape and Bi-SMA Convex Tape Booms for Deployable Membrane Structures, Journal of Mechanics Engineering and Automation, Vol.4, No.1, 52-62, 2014.
[49] Nobuhisa Katsumata, M.C. Natori, Hiroshi Yamakawa: Analysis of dynamic behaviour of inflatable booms in zigzag and modified zigzag folding patterns, Acta Astronautica, 93, 45-54, 2014.
[50] Takahira AOKI, Ken HIGUCHI, Kazuki WATANABE, SIMPLE Project Team, “Progress Report of SIMPLE Space Experiment Project on ISS Japan Experiment Module,” Trans. JSASS Aerospace Tech. Japan, Vol.12, No.ists29, pp. Tc_1-Tc_7, (2014)
[51] Takashi IWASA, Masanori HIRAMATSU, Naoko KISHIMOTO, Ken HIGUCHI, and Motoharu FUJIGAKI, “An Error Elimination Method for Surface Shape Measurement using the Grating Projection Method,” Trans. JSASS Aerospace Tech. Japan, Vol.12, pp.81-88, (2014).
[52] 岸本直子，亀井宏貴，原田 卓，岩佐貴史，樋口 健：格子投影法を用いたハニカムサンドイッチパネルの表面形状計測, 航空宇宙技術, Vol.13, pp.61-70, (2014.10.2).
----------------------------2015年度------------------------------------
[53] Takagi, S., Sakaue, Y., Uemura, T. and Takada, K.：Observation of cross-flow instability mode in yawed cylinder boundary layer at Mach 2. AIAA Journal. Vol. 53, No. 1 (2015), pp. 260-265..
[54] M. C. NATORI, Hiraku SAKAMOTO, Nobuhisa KATSUMATA, Hiroshi YAMAKAWA and Naoko KISHIMOTO: Conceptual model study using origami for membrane space structures – a perspective of origami-based engineering, Mechanical Engineering Reviews, Vol.2, No.1 (2015)
[55] S. YODA, W. CHO, R. IMAI: Aerodynamic levitator for large-sized glassy material production, Review of Scientific Instruments, Vol.86, No.9 (2015), pp. 093906-1 - 093906-5, http://dx.doi.org/10.1063/1.4930008.
[56] 岩佐貴史，岸本直子，樋口 健，藤垣元治，小木曽望：面計測と点計測を統合した大型宇宙構造物の高精度形状計測法の提案, 航空宇宙技術(AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ), Vol.14, pp.95-103, (2015.4.22). [http://doi.org/10.2322/astj.14.95]
[57] R. IMAI, K. SUZUKI, H. KAWASAKI, H. OHTA, Y. SHINMOTO, H. ASANO, O. KAWANAMI, S. MATSUMOTO, T. KURIMOTO, H. TAKAOKA, M. SAKAMOTO, K. USUKU, K. SAWADA, Development of Boiling and Two-phase Flow Experiments on board ISS (Condensation Section), Int.J. Microgravity Sci. Appl., 2016p330103 , (2016.1.31)DOI:10.15011/ijmsa.33.330103
[58] H. OHTA, H. ASANO, O. KAWANAMI, K. SUZUKI, R. IMAI, Y. SHINMOTO, S. MATSUMOTO, T. KURIMOTO, H. TAKAOKA, K. FUJII, M. SAKAMOTO, K. SAWADA, H. KAWASAKI, A. OKAMOTO, K. KOGURE, T. OKA, K. USUKU, T. TOMOBE and M. TAKAYANAGI, Development of Boiling and Two-Phase Flow Experiments on Board ISS (Research Objectives and Concept of Experimental Setup), Int. J. Microgravity Sci. Appl. 2016p330102, (2016.1.31), DOI:10.15011/ijmsa.33.330102
[59] T. GOMYO, H. ASANO, H. OHTA, Y. SHINMOTO, O. KAWANAMI, K. SUZUKI, R. IMAI, T. OKA, T. TOMOBE, K. USUKU, M. SHIMADA, S. MATSUMOTO, T. KURIMOTO, H. TAKAOKA, M. SAKAMOTO, H. KAWASAKI and K. SAWADA, Development of Boiling and Two-Phase Flow Experiments on Board ISS (Void Fraction Characteristics in the Observation Section just at the Downstream of the Heating Section), Int. J. Microgravity Sci. Appl. 2016p330104 (2016.1.31), DOI:10.15011/ijmsa.33.330104.
[60] T. HIROKAWA, D. YAMAMOTO , Y. SHINMOTO, H. OHTA, H. ASANO, O. KAWANAMI, K. SUZUKI, R. IMAI, M. TAKAYANAGI, S. MATSUMOTO, Takashi KURIMOTO, H. TAKAOKA, M. SAKAMOTO, K. SAWADA, H. KAWASAKI, K. FUJII, A. OKAMOTO, K. KOGURE, T OKA, T. TOMOBE and K. USUSKU, Development of Boiling and Two-Phase Flow Experiments on Board ISS (Investigation on Performance of Ground Model), Int. J. Microgravity Sci. Appl. 2016p330105, (2016.1.31), DOI:10.15011/ijmsa.33.330105
[61] K. SAWADA, T. KURIMOTO, A. OKAMOTO, S. MATSUMOTO, H. TAKAOKA,　H. KAWASAKI, M. TAKAYANAGI, Y. SHINMOTO, H. ASANO,　O. KAWANAMI, K. SUZUKI, R. IMAI and H. OHTA, Development of Boiling and Two-Phase Flow Experiments on Board ISS (Dissolved Air Effects on Subcooled Flow Boiling Characteristics), Int. J. Microgravity Sci. Appl. 2016p330106, (20116.1.31), DOI:10.15011/jasma.33.330106
[62] O. KAWANAMI, M. OKUBO, K. NAKAMOTO, H. ASANO, H. OHTA, Y. SHINMOTO, K. SUZUKI, R. IMAI, S. MATSUMOTO, T. KURIMOTO, H. TAKAOKA, K. SAWADA, A. OKAMOTO, H. KAWASAKI, M. TAKAYANAGI and K. FUJII, Development of Boiling and Two-Phase Flow Experiments on Board ISS (Temperature Data Derivation and Image Analysis of a Transparent Heated Short Tubein the Glass Heated Section), Int. J. Microgravity Sci. Appl. 2016p330107, (2016.1.31), DOI:10.15011/jasma.33.330107
[63] Minato, R., ”Advantage of Ethanol Fuels for Gas Generator Cycle Air Turbo Ramjet Engine” Aerospace Science and Technology Vol.50, (2016) pp.161-172.
----------------------------2016年度------------------------------------
[64] Asuka. Iijima, Daisuke Nakata, Masatoshi Sugioka, Nobuyuki Tanatsugu, Kazuyuki Higashino, Shinji Ishimoto, and Nobuyuki Azuma, “Rocket Engine Feasibility Study for the JAXA Future Transportation Reference System, ”Transactions of JSASS, Aerospace Technology Japan, Vol.14, No. ists30, pp. Po_1_17-Po_1_23, 2016.
[65］ Masazumi UEBA, Kouhei SUZAKI , and Takatoshi SUGIYAMA, “Study on Hybrid Satellite-tracking Antenna Control System Using Torque Compensation Methods for Small Vessels”, Trans. JSASS Aerospace Tech. Japan, Vol. 14, No. ists30, pp. Pj_7-Pj_12, 2016.
[66] Kazuhide MIZOBATA, Yoshihiro SUZUKI, Sakae OOISHI, Satoshi KONDOH, Takakage ARAI, and Kazuyuki HIGASHINO, “Aerodynamics and Flight Capability of a Supersonic Flight Experiment Vehicle,” Trans. JSASS Aerospace Tech. Japan, Vol. 14, No. ists30, pp. Pg_1-Pg_8, 2016.
[67] Ken HIGUCHI, Hiroshi FURUYA, Yasuyuki MIYAZAKI, Takahira AOKI, Choji YOSHIDA, Akihito WATANABE, Kazuki WATANABE and SIMPLE Project Team, “Achievement of Long-term On-orbit Operation of the SIMPLE Inflatable Extension Mast,” Trans. JSASS, Aerospace Tech. Japan, Vol. 14, No. ists30, pp. Pc_13-Pc_17, (2016).
----------------------------2017年度------------------------------------
[68] 塚野　徹，前田大輔，笹山容資，中田大将，杉岡正敏，棚次亘弘，東野和幸「 再生冷却システムに用いる熱分解吸熱性燃料に対するニッケルおよびプラチナ触媒の効果」．日本航空宇宙学会論文.第65巻2号, pp.41-49,（2017）.
[69] Masazumi Ueba, Akihiro Miyasaka, Yoshinori Suzuki, Fumihiro Yamashita, Progress in and prospects of on-board communication equipment technologies for communications satellites in Japan, accepted and to be published as IEICE Transactions Online Vol.E100-B,No.9, in Sep. 2017.
[70] Ryoji IMAI and Mori MICHIHARA, Study on Dynamic Wetting Behavior in Microgravity Condition Targeted for Propellant Tank, International Journal of Microgravity Science and Application, Vol.34, No.3, pp. 340306-1- 340306-11, (2017) DOI: 10.15011//jasma.34.340306.
[71] Kawasaki, S., Shimura, T., Uchiumi, M., and Iga, Y., “One-dimensional Analysis Method for Cavitation Instabilities of a Rotating Machinery”, 021113, Vol. 140, No. 2, J. Fluid Engineering, ASME. February 2018.
[72] Ryoji Imai, Takuya Imamura, Masatoshi Sugioka, Kazuyuki Higashino, Research on Liquid Management Technology in Water Tank and Reactor for Propulsion System with Hydrogen Production System Utilizing Aluminum and Water Reaction, Microgravity Science and Technology, online first, (2017) https://doi.org/10.1007/s12217-017-9566-5.
[73] Daisuke Nakata, Kazuki, Yasuda, Kugo Okada, Kazuyuki Higashino and Rikio Watanabe, “N2O Flow History Prediction in an Oxidizer Feed Line of Hybrid Rockets,” Transaction of JSASS, Aerospace Technology Japan, Volume 16 (2018) Issue 1 Pages 81-87, DOI: 10.2322/tastj.16.81
[74] Nagao, N., Nagaura, K., Tamura, T., Hasegawa, S., and Uchiumi, M., “Rotordynamic Forces Acting on a Two-Stage Inducer”, J. Fluid Engineering, FE-16-1588, 021112, Vol. 140, No. 2, J. Fluid Engineering, ASME, February 2018.
[75] Deployment behavior control using cables and bi-shape memory alloy convex tape booms Katsumata Nobuhisa, Kume Masaru, Higuchi Ken, ADVANCES IN MECHANICAL ENGINEERING，9巻，7号，Article Number:1687814017707909，2017年07月
[76] Kobayashi, H., Hagiwara, R., Kawasaki, S., Uchiumi, M., Yada, K., and Iga, Y., “Numerical Analysis of Suppression Effect of Asymmetric Slit on Cavitation Instabilities in Cascade”, J. Fluid Engineering, FE-16-1670, 021302, Vol. 140, No. 2, J. Fluid Engineering, ASME, February 2018.
[77] Imamura, T., Sugioka, M., Higashino, K., Imai, R., “Study on Liquid Management Technology in Water Tank for Propulsion System Utilizing Aluminum and Water Reaction (Improvement of Liquid Acquisition Performance by Hydrophilic Coating in Metallic Tank) Int. J. Microgravity Sci. Appl. Vol. 35, No. 1, p350103-1-6 (2018) DOI:10.15011//jasma.35.350103.
----------------------------2018年度------------------------------------
[78] Ikemoto, A., Inoue, T., Sakamoto, K., and Uchiumi, M., “Nonlinear Analysis of Rotordynamic Fluid Forces in the Annular Plain Seal by Using Extended Perturbation Analysis of the Bulk-Flow Theory (Influence of Whirling Amplitude in the Case With Concentric Circular Whirl)”, J. Tribology, Vol. 140, No. 4, 041708, ASME, April 2018,
[79] 向江 洋人，石原 眞優，湊 亮二郎，中田 大将，東野 和幸, 内海 政春，小型超音速機エンジン用玉軸受の発熱／冷却特性評価，ターボ機械，第46巻第6号，pp.331-337.
[80] Yuki YAMAZAKI, Kazuhide MIZOBATA, and Kazuyuki HIGASHINO, “Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology”, accepted for publication in Transactions of JSASS, Aerospace Technology Japan, Vol.16, No.ists31, 2018.
[81]Goto Keisuke, Nishimura Junpei, Kawasaki Akira, Matsuoka Ken, Kasahara Jiro, Matsuo Akiko, Funaki Ikkoh, Nakata Daisuke, Uchiumi Masaharu, Higashino Kazuyuki, Experimental Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles, Journal of Propulsion and Power, Vol. 35, No. 1 (2019), pp. 213-223. DOI: 10.2514/1.B37196,
[82]Masazumi UEBA, Yuichi TAKAKU, Kouhei TAKAHASHI, Tomohiro KAMATA , Design and Tests of Guidance and Control Systems for Autonomous Flight of a Low-speed Model Airplane for Application to a Small-scale Unmanned Supersonic Airplane, Transactions of JSASS, Aerospace Technology Japan,vol. 17, No. 2, pp.220-226, 2019
[83]Nobuyuki Azuma, Tetsuo Hiraiwa, Daisuke Ogawa, Misato Morishita, Asuka Iijima, Kazuyuki Higashino, “Deposit Formation and Heat Transfer for Bioethanol-Fueled Rocket Engine Combustion Chamber Liners” Journal of Propulsion and Power, DOI: 10.2514/1.B36887, published online 8 February 2019.
[84]Naoko KISHIMOTO, Takashi IWASA, Ken HIGUCHI, “Surface Shape Measuring Method for Space Structures Based on Images in Ultra-Violet Range, ” TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, (2018), Vol.16, No.6, pp.543-549. DOI: 10.2322/tastj.16.543.
[85]Ryojiro AKIBA, Ken HIGUCHI, Ryuichi MITSUHASHI, Riho HIRAMOTO, Jun'ya SASAKI, “Weightless Construction of High Tower to the Stratosphere, ” TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, (2018), Vol.16, No.7, pp.657-661. DOI: 10.2322/tastj.16.657.
[86] Yada, K., Uchiumi, M., and Funazaki, K., “Thomas/Alford Force on a Partial-Admission Turbine for the Rocket Engine Turbopump”, J. Fluid Engineering, 011105, Vol. 141, No. 1, ASME, January 2019.
[87] Koya Yamada, Atsushi Ikemoto, Tsuyoshi Inoue, Masaharu Uchiumi, “Nonlinear Analysis of Rotordynamic Fluid Forces in the Annular Plain Seal by Using Extended Bulk-Flow Analysis: Influence of Static Eccentricity and Whirling Amplitude”, ASME Journal of Engineering for Gas Turbines and Power, GTP-18-1412, Feb 2019, Vo1ume 41, Issue 2 : 021017, doi.org/10.1115/1.4041128
[88] 木暮大貴，井上剛志，川崎聡，内海政春，ロータダイナミック流体力の回転速度依存性を考慮した固有値解析によるLE-7A液体水素ターボポンプロータの非同期振動成分の考察，ターボ機械，第47巻第3号，pp.179-184，2019年3月．
----------------------------2019年度------------------------------------
[89] Ryoji Imai, Osamu Kawanami, Yutaka Umemura and Takehiro Himeno，“Study on break of thermal stratification in container targeted to thermodynamic vent system for future spacecraft”, IOP Conference Series: Materials Science and Engineering, Volume 502, Number 1, (2019) doi:10.1088/1757-899X/502/1/012082.
[90] 三宅建次郎，井上剛志，内海政春，池本篤史，単純ロータ系の軸振動と並行環状シールのロータダイナミック流体力の連成解析，ターボ機械，第47巻第4号，pp.227-237，2019年4月．
[91] Ryojiro Minato “Alcohol and Alkane Fuel Performance for Gas Generator Cycle Air Turbo Ramjet Engine” Aerospace Science and Technology Vol.91, (2019), pp.337-356
[92] Ryoji Imai, Kazuaki Nishida, Osamu Kawanami, Yutaka Umemura and Takehiro Himeno，“Basic study on thermodynamic vent system in propulsion system for future spacecraft”, Microgravity Science and Technology, https://doi.org/10.1007/s12217-019-09768-w, (2020)
[93] 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 投稿（Accepted）
[94] 道原 孟里・今井 良二, 推進薬タンクを対象とした微小重力下横スロッシング挙動に関する研究，Int. J. Microgravity Sci. Appl., Vol.36,No.4,pp.360403-1-10,DOI:10.15011//jasma.36.360403,(2019)
[95] Osamu Kawanami, Kentaro Takeda, Ryoma Naguchi, Ryoji Imai, Yutaka Umemura, Takehiro Himeno, Behavior of subcooling jet imjected into a bulk liquid in a tank under normal- and micro-gravity conditions，Int. J. Microgravity Sci. Appl., Vol.36,No.4,pp.360402-1-8,DOI:10.15011/jasma.36.360402, (2019).
[96] Yukiya SATO, Ryoji IMAI, Daisuke NAKATA, Ryojiro MINATO, Masaharu UCHIUMI，Study on Propellant Supply System for Small-scale Supersonic Flight Experiment Vehicle (Development of LOX Supply System design technology), Int. J. Microgravity Sci. Appl., Vol.37,No.1,pp.370104-1-7，(2020)
[97] 上羽、前田、北沢、“マルチコプターに比して短時間観測を可能とするエンジン固定翼UAVの離陸及び搭載可能重量の設計・検証”、日本航海学会論文集、Vol.140, p.41-46, 2019
[98] 渡辺、北沢、上羽、無人航空機を用いた開放地における920MHz帯の電波伝搬特性の検討、電子情報通学会誌　Ｃ, Vol.J103-C, No.1, pp.34-36, 2020
----------------------------2020年度------------------------------------
[99] 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．
[100] Ryoji Imai, KazuakiNishida, 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,
[101] 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．
[102] 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．
[103] Koki Arimatsu, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi and Masaharu Uchiumi, “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
[104] 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
[105] KazuakiNishida, 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.
[106] 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.
[107] 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 2020https://doi.org/10.2514/1.B38037Vol. 37, No. 3 (2021), pp. 419-425 doi: doi/abs/10.2514/1.B38037
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[108] Susumu HASEGAWA, Masaaki FUKUI, Yoshimasa NISHIMURA, and Kazuhide MIZOBATA,“Flow Analysis around Spaceplane for Airframe Engine Integration by CFD,” Transaction of JSASS, Aerospace Technology Japan, 2021,Volume 19,Issue 4,Pages 577-583, DOI https://doi.org/10.2322/tastj.19.577
[109] G. Coral, K. Kinefuchi, D. Nakata, R. Tsukizaki, K. Nishiyama, H. Kuninaka,Design and testing of additively manufactured high-efficiency resistojet on hydrogen propellant, Acta Astronautica (2021), doi: https://doi.org/10.1016/j.actaastro.2020.12.047. Accepted on 24th, Dec. 2020. Published online Volume 181, April 2021, Pages 14-27
[110] Daisuke Nakata, Kiyoshi Kinefuchi, Hitoshi Sakai and Suyalatu, “Thermal Design and Experimental Verification of a 3D-Printed Resistojet,” Journal of Propulsion and Power, Accepted on 25thJune, 2021 Published Online:6 Sep 2021https://doi.org/10.2514/1.B38187Published Paper: Journal of Propulsion and Power 2022 Vol.38 No.1, pp. 148–156
[111] Koichi Inoue, Haruhiko Ohta, Hitoshi Asano, Osamu Kawanami, Ryoji Imai, Koichi Suzuki, Yasuhisa Shinmoto, Takashi Kurimoto, Satoshi Matsumoto, Heat Loss Analysis of Flow Boiling Experiments Onboard International Space Station with Unclear Thermal Environmental Conditions (2nd Report: Liquid-vapor Two-phase Flow Conditions at Test Section Inlet), Microgravity Science and Technology, 2021, https://doi.org/10.1007/s12217-021-09902-7.
[112] Masazumi UEBA,Tomohiro KAMATA Sakurako NAKAJIMA, and Yosuke MAEDA,Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-SpeedModel Airplane with Application to a Small Unmanned Supersonic Airplane, Trans. JSASS Aerospace Tech. Japan,Vol. 19, No. 5, pp. 667-675, 2021,DOI: 10.2322/tastj.19.667
[113] Kiyoshi Kinefuchi, Daisuke Nakata, Giulio Coral, Suyalatu, Hitoshi Sakai, Tsukizaki Ryudo and Kazutaka Nishiyama, “Additive-manufactured single-piece thin malti-layer tungsten heater for an electrothermal thruster,” Review of Scientific InstrumentsVol.92, Issue 11, published online 9thNov., 2021, https://doi.org/10.1063/5.0068926
[114] Yasuda K, Nakata D. and Uchiumi M., Experimental Study on Temperature Change by Cavitation accompanying Self-pressurization of Propellant for Small Rocket Engines, ASME, J. Fluids Eng.Vol.143(12) 121103(2021).
[115] Naoki SOTA, Ryoji IMAI, Aoki ANADA, Taisei YAMAZAKI, Masaharu UCHIUMI,Daisuke NAKATA, and Ryojiro MINATO, Study on Propellant Supply System for a Small-scale Supersonic Flight Experiment Vehicle (Study on a Propellant Management Device), Int. J.Microgravity Sci. Appl.，Vol.38, No.1, 2021, https://doi.org/10.15011/jasma.39.390103.
[116] Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, NoboruItouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, and Jiro Kasahara, 15Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda and Kenji Maehara “Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket,” Journal of Spacecrafts and Rockets, Accepted on Oct. 25, 2021.
[117] 中村慎太郎，荒木幹也，ゴンザレスファン，山岸晃己，安田一貴，中田大将，内海政春，ハイブリッドロケットの音響放射特性，日本航空宇宙学会Accepted on 27th，Jan. 2022
[118] Matsuoka, et., al., “Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31," submitted on Jan. 2022
[119] Goto et. al., “Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31”, Journal of Spacecraft and Rockets, submitted on 23, Feb., 2022
[120] Koki Hamajima, Kei Yasukawa, Masazumi Ueba, “Design and evaluation of antenna pointing control system onboard fixed-wing UAV to realize video transmission relay station”,Accepted for publication for the IEICE Communications Express (ComEX)on 19th Jan., 2022
[121] Kei Yasukawa, Koki Hamajima, Masazumi Ueba, “Turning path tracking control technology for fixed-wing UAV to realize video transmission relay station”, Accepted for publication for the IEICE Communications Express (ComEX)on 28th Feb., 2022
[122] Satoshi Hyokawa, Masazumi Ueba, "Short-Distance Landing Control System for an 1/3-Scale Unmanned Supersonic Experimental Airplane", submitted to Aerospace Technology of Japan, on 4thFeb., 2022
[123] Sho Shimada, Masazumi Ueba, “Highly Accurate Flight-path Tracking Control System of the 1/3‑scale Unmanned Small Supersonic Aircraft to Realize a Flight from Take-off to Landing”,submitted to Aerospace Technology of Japan, on 28thFeb., 2022
[124] Kazuhide Mizobata, Taichi MIO, Katsuya MIYAMOTO, Yuki YAMAZAKI, “Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic FlightExperiment Vehicle Being Developed at Muroran Institute of Technology (SecondReport),” submitted to Transactions of JSASSon April 17, 2022.
----------------------------2022年度------------------------------------
[125] Osamu KAWANAMI, Kentaro TAKEDA, Ryoki MATSUSHIMA, Ryoji IMAI, Yutaka UMEMURA, Takehiro HIMENO, Observation of Flow Pattern and Jet-tip Height Issuing from a Nozzle at Tank Bottom in Microgravity, International Journal of Microgravity Science and Application, Vol.39, No. 2, 2022, https://doi.org/10.15011/jasma.39.390201.