研究業績

A.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(室蘭工業大学大学院),中田大将,杉岡正敏,棚次亘弘,東野和幸(室蘭工業大学)「 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.

B.国際学会発表論文

under construction

C.国内学会発表論文

under construction

D.紀要等

under construction