研究者業績
基本情報
- 所属
- 国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 名誉教授東京理科大学 客員教授
- 学位
- 工学博士(航空学)(東京大学)
- 連絡先
- fujii
rs.tus.ac.jp - 通称等の別名
- Ko Fujii
- J-GLOBAL ID
- 200901042342169670
- researchmap会員ID
- 1000144496
- 外部リンク
経歴
19-
2023年10月 - 現在
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2015年4月 - 現在
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2015年4月 - 2023年9月
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2013年4月 - 2015年3月
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2003年10月 - 2015年3月
学歴
2-
- 1980年
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- 1974年
委員歴
14-
2020年10月 - 2026年9月
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2011年4月 - 2026年3月
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1991年4月 - 2026年3月
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2021年1月 - 2023年3月
受賞
32-
2024年7月
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2023年6月
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2023年3月
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2023年2月
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2022年9月
論文
433-
Flow, Turbulence and Combustion 2025年7月2日 査読有り招待有り筆頭著者<jats:title>Abstract</jats:title> <jats:p>Scale-resolving simulations possess considerable benefits over modeled approaches because of their ability to access the underlying nonlinear fluid dynamics, and thus to predict not only the correct phenomenology, but also to generate insights on strategies to mitigate or eliminate undesirable features. The expense of resolving all pertinent turbulent scales becomes prohibitive however, as the size of the problem, typically measured by the Reynolds number based on a suitable set of reference parameters, becomes large, as is the case with flows of industrial interest such as full aircraft or their complex subsystems. This paper provides an assessment of scale-resolving methods, including some of the main benefits as well as barriers for use on large problems, together with a perspective on historical and recent trends that appear promising in the quest for routine industrial use. The factors that constitute the biggest hurdles to achieving acceptable wall-clock times and costs include meshing of complicated geometries, numerical schemes that are robust as well as accurate, suitable initial and boundary conditions, economical yet appropriate representation of near-wall turbulence, code parallelism, scalability and portability, and post-processing of the resulting big datasets. Considerations for these interrelated aspects are highlighted in the context of several 3D problems of increasing complexity, from wing sections without and with sweep, to aircraft wakes, propulsion subsystems, scramjet flowpaths and finally, full aircraft including empennages. Collectively, these examples feature the benefits of scale-resolving simulations. An illustrative approach that has reached a relatively high level of maturity using automatic mesh generation, a non-dissipative yet robust scheme, wall-modeling of turbulence, superior scalability and requiring little user intervention beyond providing the surface model, is used to demonstrate the potential of scale-resolving simulations for industry, achievable at modest cost and in reasonable wall-clock time.</jats:p>
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IEEE Access 13 39631-39649 2025年 査読有り
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Proceedings of the Cambridge Unsteady Flow Symposium 2024 257-271 2024年12月3日 査読有り招待有り
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Aerospace 11(11) 866-866 2024年10月22日 査読有りThe advancement of Arrival MANager (AMAN) is crucial for addressing the increasing complexity and demand of modern airspace. This study evaluates the operational feasibility and effectiveness of an innovative AMAN designed for en route airspace, the so-called En Route AMAN. The En Route AMAN functions as a controller support system, facilitating the sharing of information between en route air traffic controllers (ATCos), approach controllers (current AMAN), and airport controllers (Departure Managers) in airports with multiple runways. The En Route AMAN aims to support upstream ATCos by sequencing and spacing of incoming streams via speed control and runway assignment, thereby enhancing overall air traffic efficiency. Human-In-The-Loop simulations involving rated ATCos are performed under scenarios that replicate real-world traffic and weather conditions. These simulations focus on upstream airspace to assess the impact of En Route AMAN on delay mitigation and ATCos’ performance. Unlike previous studies that solely relied on theoretical models and fast-time simulation for operational feasibility evaluation, this approach incorporates ATCos’ real-time decision-making, situational awareness, and task management, addressing critical operationalization challenges. The results demonstrated that the En Route AMAN could reduce the average flight duration by up to 25.6 s and decrease the total number of ATCo instructions by up to 20% during peak traffic volume. These findings support that the En Route AMAN is both operationally viable and effective in mitigating arrival delays, highlighting the importance of Human-In-The-Loop for practical validation.
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AIAA SCITECH 2024 Forum 2024年1月4日
MISC
191-
日本機械学会論文集. B編 63(610) 1902-1907 1997年6月25日In this paper, we describe the flow structure of a cavity interacting with a normal shock wave in a supersonic duct. The position of the normal shock wave and the bleed inside the cavity are focused on. Experiments are conducted at Mach number M=1.58. Time-averaged and unsteady pressures are measured and the flows are visualized by the schlieren and the oil flow techniques. The characteristics of the cavity flow with a shock wave interaction, namely, a shock system around the cavity and the separation in the interacting region are recognized. The bleed inside the cavity stabilizes the normal shock wave.
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International Journal of Computational Fluid Dynamics 8 235-246 1997年
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計算工学 = Journal of The Japan Society for Computational Engineering and Science (JSCES) 1(3) 163-167 1996年9月30日
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日本機械学会論文集. B編 61(586) 2136-2142 1995年6月25日In this work, the wavefront of a compression wave generated by a train moving into a tunnel is studied. A new one-dimensional flow model in which the flow around the train is considered to be a stream tube is proposed to determine the key parameters that affect the wavefront of the compression wave. From the result, the wavefront is found to be proportional to the lateral velocity at the height of the tunnel wall in steady flow around the train before the train enters the tunnel. This relationship between the wavefront and the velocity of the steady flow is validated from the experimental data. The result indicates that the wavefront of the compression wave can be predicted by investigating the steady flow field around the train in stead of the unsteady flow when the train moves into a tunnel.
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AIAA JOURNAL 25(3) 369-370 1987年3月
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航空宇宙技術研究所特別資料 7 289-298 1986年
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航空宇宙技術研究所報告 889 1-18 1985年
書籍等出版物
31-
Cambridge University Press 2015年4月
講演・口頭発表等
1066-
AJK FED2023(ASME-JSME-KSME Joint Fluids Engineering Conference) 2023年7月9日
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AJK FED2023(ASME-JSME-KSME Joint Fluids Engineering Conference) 2023年7月9日
所属学協会
11Works(作品等)
20共同研究・競争的資金等の研究課題
28-
日本学術振興会 科学研究費助成事業 2018年4月 - 2021年3月
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日本学術振興会 科学研究費助成事業 2017年11月 - 2019年3月
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ポスト「京」で重点的に取り組むべき社会的・科学的課題に関するアプリケーション開発・研究開発 萌芽的課題研究 2016年8月 - 2019年3月
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日本学術振興会 科学研究費補助金基盤A 2015年4月 - 2018年3月
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日本学術振興会 科学研究費助成事業 2012年4月 - 2015年3月