Curriculum Vitaes
Profile Information
- Affiliation
- Professor of Emeritus, Institute of Space and Astronautical Science, Japan Aerospace Exploration AgencyVisiting Professor, Tokyo University of Science
- Degree
- Doctor of Engineering(The University of Tokyo)
- Contact information
- fujii
rs.tus.ac.jp
- Other name(s) (e.g. nickname)
- Ko Fujii
- J-GLOBAL ID
- 200901042342169670
- researchmap Member ID
- 1000144496
- External link
Major Research Interests
4Research Areas
2Research History
19-
Apr, 2015 - Present
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Apr, 2015 - Sep, 2023
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Apr, 2013 - Mar, 2015
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Oct, 2003 - Mar, 2015
Education
2Committee Memberships
14-
Oct, 2020 - Sep, 2026
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Jul, 2016 - Jul, 2024
Awards
32-
Jun, 2023
Papers
433-
Flow, Turbulence and Combustion, Jul 2, 2025 Peer-reviewedInvitedLead author<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 Peer-reviewed
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Proceedings of the Cambridge Unsteady Flow Symposium 2024, 257-271, Dec 3, 2024 Peer-reviewedInvited
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Aerospace, 11(11) 866-866, Oct 22, 2024 Peer-reviewedThe 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, Jan 4, 2024
Misc.
191-
Proceedings of the conference on computational engineering and science, 3(1) 109-112, May 26, 1999
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Special publication of National Aerospace Laboratory : SP, 37 223-228, 1998
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Special publication of National Aerospace Laboratory : SP, 37 283-288, 1998
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日本航空宇宙学会年会講演会講演集, 29th 60-61, 1998
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Transactions of the Japan Society of Mechanical Engineers. Series B., 63(610) 1902-1907, Jun 25, 1997In 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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Special publication of National Aerospace Laboratory : SP, 34 147-152, 1997
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Special publication of National Aerospace Laboratory : SP, 34 257-262, 1997
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International Journal of Computational Fluid Dynamics, 8 235-246, 1997
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Proceedings of the conference on computational engineering and science, 1(1) 209-212, May 29, 1996
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Proceedings of the conference on computational engineering and science, 1(1) 287-290, May 29, 1996
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Proceedings of the conference on computational engineering and science, 1(1) 283-286, May 29, 1996
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Proceedings of the conference on computational engineering and science, 1(1) 279-282, May 29, 1996
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Special publication of National Aerospace Laboratory : SP, 30 99-104, 1996
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Transactions of the Japan Society of Mechanical Engineers. Series B., 61(586) 2136-2142, Jun 25, 1995In 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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Special publication of National Aerospace Laboratory : SP, 22 203-208, 1994
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Special publication of National Aerospace Laboratory : SP, 27 159-164, 1994
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Journal of the Japan Society of Mechanical Engineers, 96(895) 474-478, Jun 5, 1993
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Special publication of National Aerospace Laboratory : SP, 19 109-114, 1992
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Special publication of National Aerospace Laboratory : SP, 19 81-86, 1992
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Special publication of National Aerospace Laboratory : SP, 19 115-120, 1992
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Special publication of National Aerospace Laboratory : SP, 16 129-134, 1991
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Special publication of National Aerospace Laboratory : SP, 14 127-132, 1990
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AIAA JOURNAL, 25(3) 369-370, Mar, 1987
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Special publication of National Aerospace Laboratory : SP, 8 13-18, 1987
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Special publication of National Aerospace Laboratory : SP, 8 85-90, 1987
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Special publication of National Aerospace Laboratory : SP, 7 249-254, 1986
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Special publication of National Aerospace Laboratory : SP, 7 299-314, 1986
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Special publication of National Aerospace Laboratory : SP, 7 289-298, 1986
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Special publication of National Aerospace Laboratory : SP, 7 53-60, 1986
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Technical report of National Aerospace Laboratory, 889 1-18, 1985
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Special publication of National Aerospace Laboratory : SP, 5 167-174, 1985
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Special publication of National Aerospace Laboratory : SP, 5 159-166, 1985
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Special publication of National Aerospace Laboratory : SP, 3 27-34, 1984
Books and Other Publications
31-
Cambridge University Press, Apr, 2015
Presentations
1066-
AJK FED2023(ASME-JSME-KSME Joint Fluids Engineering Conference), Jul 9, 2023
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AJK FED2023(ASME-JSME-KSME Joint Fluids Engineering Conference), Jul 9, 2023
Professional Memberships
11Works
20Research Projects
28-
Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2018 - Mar, 2021
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Nov, 2017 - Mar, 2019
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萌芽的課題研究, 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, Aug, 2016 - Mar, 2019
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科学研究費補助金基盤A, 日本学術振興会, Apr, 2015 - Mar, 2018
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2012 - Mar, 2015