2009 Fiscal Year Final Research Report
Fundamental Research for Silent Supersonic Transport Based on Supersonic Biplane Theory
| Project/Area Number |
19206086
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| Research Category |
Grant-in-Aid for Scientific Research (A)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Tohoku University |
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Principal Investigator |
OBAYASHI Shigeru Tohoku University, 流体科学研究所, 教授 (80183028)
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| Co-Investigator(Kenkyū-buntansha) |
ASAI Keisuke 名古屋大学, 大学院・工学研究科, 教授 (40358669)
NAGAI Hiroki 東北大学, 大学院・工学研究科, 准教授 (70360724)
SASOU Akihiro 東北大学, 大学院・工学研究科, 教授 (40215752)
KAWAZOE Hiromitsu 鳥取大学, 大学院・工学研究科, 教授 (40260591)
MATSUNO Takashi 鳥取大学, 大学院・工学研究科, 講師 (90432608)
NAKAHASHI Kazuhiro 東北大学, 大学院・工学研究科, 教授 (00207854)
MATSUSHIMA Kisa 富山大学, 大学院・理工学研究部, 教授 (40332514)
JEONG Shinkyu 東北大学, 流体科学研究所, 准教授 (20358469)
TSUBOI Nobuyuki 九州工業大学, 大学院・工学研究院, 准教授 (40342620)
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| Co-Investigator(Renkei-kenkyūsha) |
NAKAMURA Yoshiaki 名古屋大学, 大学院・工学研究科, 教授 (80115609)
MIYAJI Kouji 横浜国立大学, 工学研究院, 准教授 (60313467)
SATO Tetsuya 早稲田大学, 理工学術院, 教授 (80249937)
MATSUO Akiko 慶応義塾大学, 理工学部, 教授 (70276418)
SAWAI Syujiro 独立行政法人宇宙航空研究開発機構, 宇宙科学研究本部, 准教授 (30270440)
FUJITA Kazuhisa 独立行政法人宇宙航空研究開発機構, 総合技術研究本部・空気力学研究グループ, 准教授 (90281584)
KOBAYASHI Hiroaki 独立行政法人宇宙航空研究開発機構, 総合技術研究本部航空エンジン技術開発センター・航空エンジン技術開発センター, 准教授 (50353420)
TAGUCHI Hideyuki 独立行政法人宇宙航空研究開発機構, 航空プログラムグループ・超音速機チーム・宇宙科学研究本部, 主任研究員 (90358515)
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| Project Period (FY) |
2007 – 2009
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| Keywords | 超音速流れ / 数値流体力学 / 風洞実験 / ソニックブーム |
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| Research Abstract |
Supersonic Biplane Theory is a concept of eliminating wave drag and sonic boom by using shock wave interaction between two airfoils facing each other. The following research topics are investigated in this research to construct and validate the theory : Definition of three-dimensional wing configuration and its optimization, Investigation of low speed characteristics of supersonic biplane by using CFD and EFD, Supersonic wind tunnel test of starting process of three-dimensional supersonic biplane, Free flight experiment of supersonic biplane using ballistic range.
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Research Products
(41 results)
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[Journal Article] Impulse Generation Mechanisms in Laser-Driven In-Tube Accelerator2008
Author(s)
Choi, J.-Y., Sasoh, A., Jeung, I.-S., Urabe, N., Kleine, H.
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Journal Title
Transactions of The Japan Society for Aeronautical and Space Sciences Vol.51, No.172
Pages: 71-77
Peer Reviewed
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[Presentation] Development status of a hypersonic precooled turbojet engine2009
Author(s)
Tetsuya Sato, Hideyuki Taguchi, Hiroaiki Kobayashi, Takayuki Kojima, Kenya Harada, Motoyuki Hongoh, Daisaku Masaki, Keiichi Okai, Kazuhisa Fujita, Shujiro Sawai
Organizer
60th International Astronautical Congress
Place of Presentation
Daejeon Conference Centre, Daejeon, Korea
Year and Date
20091012-20091016
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[Presentation] Optical Fiber Sensor Capable of Measuring Pressure and Temperature from Luminescent Lifetime2009
Author(s)
Sugai, N., Yorita, D., Numata, D., Nagai, H., Asai, K.
Organizer
6th International Conference on Flow Dynamics
Place of Presentation
Hotel Metropolitan Sendai, Japan
Year and Date
2009-11-06
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[Presentation] Three dimensional effect of a supersonic busemann biplane on start process2009
Author(s)
NAGAI, H., OYAMA, S., ASAI, K., FUJISONO, T., OBAYASHI, S.
Organizer
27th International Symposium on Space Technology and Science
Place of Presentation
Tsukuba International symposium, Japan
Year and Date
2009-07-10
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[Presentation] Development Status of A Precooled Turbojet Engine2009
Author(s)
Tetsuya Sato, Hideyuki Taguchi, Hiroaiki Kobayashi, Takayuki Kojima, Motoyuki Hongoh, Kenya Harada, Daisaku Masaki, Keiichi Okai, Kazuhisa Fujita, Shujiro Sawai
Organizer
27th International Symposium on Space Technology and Science
Place of Presentation
Tsukuba International Congress Center, Tsukuba, Japan
Year and Date
2009-07-08
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[Presentation] Experimental Study on Interference Flow of a Supersonic Busemann Biplane using Pressure-Sensitive Paint Technique2008
Author(s)
NAGAI, H., OYAMA, S., OGAWA, T., KURATANI, N., ASAI, K.
Organizer
Proceedings of the International Council of the Aeronautical Sciences
Place of Presentation
William A. Egan Civic & Convention Centre, Anchorage, Alaska, USA
Year and Date
2008-09-17
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[Presentation] Forebody Vortex Control on High Performance Aircraft Using PWM-Controlled Plasma Actuators2008
Author(s)
Matsuno, T., Kawazoe, H., Nelson, R. C., Corke, T. C.
Organizer
Proceedings of the 26th International Congress of the Aeronautical Sciences
Place of Presentation
William A. Egan Civic & Convention Centre, Anchorage, Alaska, USA(CDROM)
Year and Date
2008-09-15
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[Presentation] Visualization of Interacting Flow Field between Busemann's Biplane in Supersonic Flow2008
Author(s)
KURATANI, N., NAGAI, H., ASAI, K., OGAWA, T., OBAYASHI, S.
Organizer
Proceedings of the 13th International Symposium on Flow Visualization
Place of Presentation
Acropolis Convention Center, Nice, France
Year and Date
2008-07-01
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