Achievement

2024 |2023 | 2022 | 2021 | 2020 | 2019 | 2018 |2017 |2016 |2015 | 2014 | 2013 | 2012 | 2011 | 2010 | 2009- | 　　　　

2024

  • 1. K. Sekine, D.Iwata, P. Bouchaudon, T. Tatsukawa, K. Fujii, K. Tominaga, E. Itoh, ” Validating a Flow-based Arrival Management for En Route Airspace: A Human-in-the-Loop Simulation Experiment with ESCAPE Light Simulator”, Aerospace, Vol.11, No.11, Oct. 2024.; https://doi.org/10.3390/aerospace11110866

2023

  • 1. Y. Abe, T. Nonomura, M. Sato, H. Aono, K. Fujii, “Comparison of separation control mechanisms for synthetic jet and plasma actuator”, Vol. 12, No. 8, Actuators, Aug. 2023. ; https://doi.org/10.3390/act12080322
  • 2. K. Sekine, F. Kato, T. Tatsukawa, K. Fujii and E. Itoh, “Rule Design for Interpretable En Route Arrival Management via Runway-Flow and Inter-Aircraft Control”, IEEE Access, Jul. 2023. ; https://doi.org/10.1109/ACCESS.2023.3297136
  • 3. Y. Abe, T. Nonomura, K. Fujii, “Flow instability and momentum exchange in separation control by a synthetic jet”, Physics of Fluids, Vol. 35, Issue 6, 065114(2023). June 2023. ; https://doi.org/10.1063/5.0148943

2022

  • 1. S. Sekimoto, K. Fujii, M. Anyoji, Y. Miyakawa, S. Ito, S. Shimomura, H. Nishida, T. Nonomura, T. Matsuno, “Flow Control around a NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of　Reynolds Number”, Actuators, Vol. 12, No.43, Jan. 2023. ; https://doi.org/10.3390/act12010043
  • 2. T. Ogawa, K. Asada, M. Sato, T. Tatsukawa, K. Fujii, “Computational Study of the Plasma Actuator Flow Control for an Airfoil at Pre-stall Angles of Attack”, Applied Sciences, Vol. 12, Iss. 18, Sep. 2022. ; https://doi.org/10.3390/app12189073
  • 3. D. Terakado, T. Nonomura, H. Aono, M. Sato, A. Oyama and K. Fujii, “Sound source characteristics generated by shocklets in isotropic compressible Turbulence”, Physical Review Fluids, Vol.7, Iss. 8, Aug. 2022. ; https://doi.org/10.1103/PhysRevFluids.7.084605
  • + 3 journal articles in Japanese

2021

  • 1. S. Sekimoto, H. Kato, K. Fujii, H. Yoneda, “In-Flight Demonstration of Stall Improvement Using a Plasma Actuator for a Small Unmanned Aerial Vehicle”, Aerospace, Vol. 9, No. 3, Mar. 2022 ; https://doi.org/10.3390/aerospace9030144
  • 2. T. Ogawa, K. Asada, S. Sekimoto, T. Tatsukawa and K. Fujii, “Dynamic Burst Actuation to Enhance the Flow Control Authority of Plasma Actuators", Aerospace, Vol. 8, No. 12, Dec. 2021 ; DOI: https://doi.org/10.3390/aerospace8120396
  • 3. W. Obayashi, H. Aono, T. Tatsukawa, K. Fujii , “Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder”, AIP Advances, Vol. 11, Issue. 10, pp.105211.1-105211.6, Oct. 2021, ;DOI: https://doi.org/10.1063/5.0065637
  • 4. T. Nonomura, Y. Ozawa, Y. Abe and K. Fujii, “Computational Study on Aero-acoustic Fields of a Transitional Supersonic Jet”, The Journal of the Acoustical Society of America, Vol. 149, Issue 6, pp.4484-4502, June 2021; DOI: https://doi.org/10.1121/10.0005313
  • 5. K. Sekine, T. Tatsukawa, K. Fujii and E. Itoh, “Multi-objective takeoff time optimization using cellular automaton-based simulator”, IEEE Access , Vol. 9, pp. 79461-79476, May 2021. ; DOI: https://doi.org/10.1109/ACCESS.2021.3084215
  • + 4 journal articles in Japanese

2020

  • 1. D. Chen, K. Asada, S. Sekimoto, K. Fujii, and H. Nishida,“A high-fidelity body-force modelling approach for plasma-based flow control simulations”, Physics of Fluids, accepted for publication, Feb. 2021. ; doi: https://doi.org/10.1063/5.0040987.
  • 2. T. Abe, K. Asada, S. Sekimoto, K. Fukudome, H. Mamori, T. Tatsukawa, K. Fujii, and M. Yamamoto, “Computational Study of Wing Tip Effect for the Flow Control Authority of DBD Plasma Actuator, AIAA Journal, Vol. 59, No. 1, pp. 104-117 2021; doi: doi/abs/10.2514/1.J059706.
  • 3. S. Shimomura, S. Sekimoto, A. Oyama, K. Fujii, H. Nishida, “Closed-Loop Flow Separation Control Utilizing the Deep Q-Network over Airfoill”, AIAA Journal, Vol. 58, No. 10, pp. 4243–4259, 2020; https://doi.org/10.2514/1.J059254.
  • 4. S. Sekimoto, K. Fujii, S. Hosokawa, H. Akamatsu, “Flow-control Capability of Electronic-substrate-sized Power Supply for a Plasma Actuator”, Sensors & Actuators: A Physical, Elsevier, Vol. 306, No. 1, May 2020, 11951, https://doi.org/10.1016/j.sna.2020.111951.
  • 5. H. Aono, H. Fukumoto, Y. Abe, M. Sato, T. Nonomura, K. Fujii, “Separated Flow Control of Small Horizontal-Axis Wind Turbine Blades Using Dielectric Barrier Discharge Plasma Actuators,” Energies, a Section of Electrical Power and Energy System, MDPI, Vol. 13, Issue 5, 2020; https://doi.org/10.3390/en13051218.
  • + 2 journal articles in Japanese

2019

  • 1. M. Sato, K. Okada, K. Asada, H. Aono, T. Nonomura, and K. Fujii, “Unified Mechanisms for Separation Control around Airfoil using Plasma Actuator with Burst Actuation over Reynolds Number Range of 103-106,” Physics of Fluids, Vol. 32, Issue 2, Feb. 2020. (editor’s pick); https://doi.org/10.1063/1.5136072
  • 2. H. Sato, S. Kimura, I. Ueno, H. Suzuki T. Tatsukawa, K. Fujii, M. Yamamoto, C. Mukai “Space Educational Program of the Tokyo University of Science: A Trial for Space Education”, Transactions of The Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, pp. 25-32, Vol. 17, No. 1, Jan. 2019
  • 3. H. Aono, K. Kondo, T. Nonomura, M. Anyoji, A. Oyama, K. Fujii and M. Yamamoto, “Aerodynamics of owl-like wing model at low Reynolds numbers,” Vol. 63, No. 1, pp. 8-17, Transactions of JSASS, Jan. 2020; https://doi.org/10.2322/tjsass.63.8
  • 4. K. Shimizu, T. Nakajima, S. Sekimoto, K. Fujii, T. Hiraoka, Y. Nakamura, T. Nouzawa, J. Ikeda and M. Tsubokura, “Aerodynamic drag reduction of a simplified vehicle model by promoting flsw separation using plasma actuator, JSME Mechanical Engineering Letters, Bulletin of the JSME, Vol.5, No. 19-00354, 2019. DOI; https://doi.org/10.1299/mel.19-00354
  • 5. T. Nonomura, H. Nakano, Y. Ozawa, D. Terakado, M. Yamamoto, K. Fujii, A. Oyama, “Large Eddy Simulation of Acoustic Waves Generated from a Hot Supersonic Jet”, Shock Wave, Vol. 29, pp. 1133-1154, 2019 ; https://doi.org/10.1007/s00193-019-00895-2
  • + 3 journal articles in Japanese

2018

  • 1. S. Kawai, T. Bouwhuis, Y. Abe, A. Yakeno, T. Nonomura, H. Aono, A. Oyama, H. W. M Hoeijmakers, K. Fujii, “Dominant Parameters for Maximum Velocity Induced by Body-force Models for Plasma Actuators”, Theoretical and Computational Fluid Dynamics, pp 805–820, Vol. 32, Issue 6, December 2018; https://link.springer.com/article/10.1007/s00162-018-0478-9.
  • 2. A. Yakeno, Y. Abe, S. Kawai, T. Nonomura, and K. Fujii, “Unsteady shear layer flow under excited local body-force for flow-separation control in downstream of a two-dimensional hump”, International Journal of Heat and Fluid Flow, Vol. 74, pp. 15-27, 2018; DOI: 10.1016/j.ijheatfluidflow.2018.08.008.
  • 3. Y. Ozawa, T. Nonomura, M. Anyoji, H. Mamori, N. Fukusima, A.Oyama, K. Fujii, and M. Yamamoto, “Identification of Acoustic Wave Propagation Pattern of a Supersonic Jet Using Frequency-Domain POD”, Research Note, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 61, No. 6, pp. 281-284, 2018; DOI: https://doi.org/10.2322/tjsass.61.281
  • 4. S. Morizawa, T. Nonomura, A. Oyama, K. Fujii and S. Obayashi, “Effect of Mach Number on Airfoil Characteristics at Reynolds Number of 3,000”, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 61, No. 6, pp. 258-267, 2018; DOI: https://doi.org/10.2322/tjsass.61.258．
  • 5. K. Fujii, “Three Flow Features behind the Flow Control Authority of DBD　Plasma Actuator”, Applied Science, 8 (4), 546, April 2018; DOI:10.3390/app8040546.

2017

  • 1. H. Aono, S. Kawai, T. Nonomura, M. Sato, K. Fujii and K. Okada, “Plasma-Actuator Burst-Mode Frequency Effects on Leading-Edge Flow-Separation Control at Reynolds Number 2.6·105,” AIAA Journal, Vol.55, pp. 3789-3806, 2017.
  • 2. S. Sekimoto, T. Nonomura, and K. Fujii, "Burst-Mode Frequency Effects of Dielectric Barrier Discharge Plasma Actuator for Separation Control". AIAA Journal, Vol. 55, No. 4, pp. 1385-1392, 2017, DOI: 10.2514/1.J054678
  • 3. T. Nonomura, and K. Fujii, “Characteristic finite-difference WENO scheme for multicomponent compressible fluid analysis: Overestimated quasi-conservative formulation maintaining equilibriums of velocity, pressure, and temperature”, Journal of Computational Physics, Vol. 340, pp. 358-388, January 2017, DOI: https://doi.org/10.1016/j.jcp.2017.02.054
  • 4. M. Sato, K. Asada, S. Kawai, T. Nonomura, and K. Fujii, “Large-Eddy Simulation of NACA0015-Airfoil Flow at Reynolds Number of　1.6 × 106,” AIAA Journal, TN, Vol. 55, No. 2, pp. 673-679, 2017, DOI:10.2514/1.J054963
  • 5. D. Lee, T. Nonomura, A. Oyama, and K. Fujii, “Comparative Studies of Numerical Methods for Evaluating Aerodynamic Characteristics of Two-Dimensional Airfoil at Low Reynolds Numbers,” International Journal of Computational Fluid Dynamics, Vol. 31, pp. 57-67, 2017.DOI: 10.1080/10618562.2016.1274398
  • + 2 journal articles in Japanese

2016

  • 1. Y. Ozawa, A. Oyama, M. Anyoji, H. Mamori, N. Fukushima, M. Yamamoto and K. Fujii, “Analysis of nozzle geometry effect on supersonic jet noise using Schlieren,” The Journal of the Acoustical Society of America, Vol. 140, No. 4, 3043, 2016. DOI: http://dx.doi.org/10.1121/1.4969449
  • 2. A. Yakeno, S. Kawai, T. Nonomura, and K. Fujii, “Wall-Turbulence Structure with Pressure Gradient around 2D Hump”, Progress in Turbulence, Vol. VI, pp. 167-170, 2016.DOI: 10.1007/978-3-319-29130-7_30
  • 3. A. Yakeno, Y, Abe, S. Kawai, T. Nonomura and K. Fujii,“Spanwise Modulation Effects of Local Body Force on Downstream Turbulence Growth around Two-Dimensional Hump,” International Journal of Heat and Fluid Flow, Vol. 55, pp. 52-64, 2016，DOI: 10.1016/j.ijheatfluidflow.2016.11.012
  • 4. D. Kato, Y. Abe, T. Nonomura, A. Oyama, K. Fujii, T. Ikeda and M. Koishi, “Computational Analysis of Aeroacoustic Noise Generated from a Rotating Tire with a Longitudinal Groove,” The Journal of the Acoustical Society of America, Vol. 140, No. 4, 2016. DOI: 10.1121/1.4971058
  • 5. T. Tatsukawa, T. Nonomura, A. Oyama, and K. Fujii. "Multi-Objective Aeroacoustic Design Exploration of Launch-Pad Flame Deflector Using Large-Eddy Simulation", Journal of Spacecraft and Rockets, Vol. 53, No. 4, pp. 751-758, 2016.DOI: http://dx.doi.org/10.2514/1.A33420
  • 6. H. Fukumoto, H. Aono, T. Watanabe, N, Tanaka, H. Matsuda, T. Ohsako, T. Nonomura, A. Oyama, and K. Fujii, “Control of Dynamic Flowfield around a Pitching NACA633-618 Airfoil by a DBD Plasma Actuator,” International Journal of Heat and Fluid Flow, Vol. 62, Part A, pp. 10–23, 2016. DOI: 10.1016/j.ijheatfluidflow.2016.10.012
  • 7. T. Nonomura, H. Honda, Y. Nagata, M. Yamamoto, S. Morizawa, S. Obayashi, K. Fujii, Plate-Angle Effects on Acoustic Waves from Supersonic Jets Impinging on Inclined Plates,” AIAA Journal, Vol.54, No. 3 pp. 816-827. 2016. DOI: 10.2514/1. J054152
  • 8. Terakado, D., Nagata, Y., Nonomura, T., K., Fujii, and M., Yamamoto, “Computational Analysis of Compressible Gas-particle-multiphase Turbulent Mixing Layer in Euler-Euler Formulation,”, Transactions of The Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 14, ists30, pp.25-31, 2016, ; DOI: 10.2322/tastj.14.Po_2_25
  • 9. Morizawa, S., Nonomura, T., Obayashi, S., Oyama, A., Fujii, K., “Multiobjective Design Exploration of Propeller Airfoils at Low-Reynolds and High-Mach Number Conditions towards Mars Airplane,”, Transactions of The Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 14, ists30, pp.47-53, 2016, ; DOI: 10.2322/tastj.14.Pk_47

2015

  • 1. Y. Abe, T. Haga, T. Nonomuraand K. Fujii, “Conservative high-order flux-reconstruction schemes on moving and deforming grids,” Computers & Fluids, Vol. 139, No. 5, pp. 2-16, 2015. https://doi.org/10.1016/j.compfluid.2016.03.024
  • 2. C. Bailly, and K. Fujii, “High-speed jet noise”, Mechanical Engineering Review, JSME: DOI:10.1299/MER.15-00496, Nov. 27, 2015.
  • 3. K. Fujii, “Computational studies on flow separation controls at relatively low Reynolds number regime,” Advances in computation, modeling and control of transitional and turbulent flows, Ed. by Sengupta, T., Lele, S. K. and Davidson, P. A., World Scientifi, Nov. 2015.
  • 4. M. Sato, H. Aono, A. Yakeno, T. Nonomura, K. Fujii, K. Okada, and K. Asada, “Multifactorial effects of operating conditions of dielectric-barrier-discharge plasma actuator on laminar-separated-flow control,” AIAA Journal, Vol.53, No.9, pp. 2544-2559, 2015.
  • 5. W. Li, T. Nonomura, and K. Fujii, “Generation of acoustic disturbances in supersonic laminar cavity flows,” International Journal of Acoustics and Vibration Vol.20, No. 3, pp. 135-142, 2015.
  • 6. H. Aono, S. Sekimoto, M. Sato, A. Yakeno, T. Nonomura, and K. Fujii, “Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air,” Bulletin of the JSME Mechanical Engineering Journal Vol. 2, No. 4 pp. 1-16 2015.
  • 7. A. Yakeno, S. Kawai, T. Nonomura, and K. Fujii,“Separation-control based on turbulence transition around 2D hump at different Reynolds numbers,” International Journal of Heat and Fluid Flow, Vol. 55, pp. 52-64 2015. 　 　
  • 8. Y. Abe, K. Okada, T. Nonomura, and K. Fujii, “The effects of actuation frequency on the separation control over an airfoil using a synthetic jet,” Progress in Flight Physics, TORUS PRESS, Vol.7, pp.147-168 2015.
  • 9. M. Sato, T. Nonomura, K. Okada, K. Asada, H. Aono, A. Yakeno, Y. Abe, and K. Fujii, “Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number,” Physics of Fluids Vol. 27 (117101) 2015.
  • 10. K. Asada, T. Nonomura, H. Aono, M. Sato, K. Okada, and, K. Fujii, “LES of transient flows　controlled by DBD plasma　actuator over a stalled　airfoil,” International Journal of　Computational Fluid Dynamics Vol. 29, pp. 215-229 2015.
  • 11. D. Lee, Nonomura, T., Oyama, A. and Fujii, K., “Comparison of numerical methods evaluating airfoil aerodynamic characteristics at low Reynolds number,” Journal of Aircraft Vol. 52, No. 1, pp. 296-306 2015.
  • 12. D. Lee, Kawai, S., Nonomura, T., Anyoji, M., Aono, H., Oyama, A., Asai, K. and Fujii, K., “Mechanisms of surface pressure distribution within a laminar separation bubble at different Reynolds numbers,” Physics of Fluids Vol. 27 (023602) 2015.
  • 13. Y. Abe, T. Haga, T. Nonomura, and K. Fujii, “On the freestream preservation of high-order conservative flux-reconstruction schemes,” Journal of Computational Physics Vol.281, pp. 28-54 2015.
  • 14. N. Fujioka, T. Nonomura, A. Oyama, M. Yamamoto and K. Fujii, “Computational Analysis of Aerodynamic Performance of Mars Airplane,” The Japan Society of Aeronautical and Space Sciences, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 12, Ists29, pp.1-5. 2014
  • + 4 journal articles in Japanese

2014

  • 1. T. Nonomura, D. Terakado, Y. Abe, and K. Fujii, “A new technique for freestream preservation of finite-difference WENO on curvilinear grid,” Computers & Fluids 107 (2015) 242–255 2015.
  • 2. Anyoji, M., Nonomura, T., Aono, H., Oyama, A., Fujii, K., Nagai H. and Asai, K., “Computational and experimental analysis of a high-performance airfoil under low-Reynolds-number flow condition,” Journal of Aircraft, 2014.
  • 3. Fujii, K., “High-performance computing-based exploration of flow control with micro devices,” Philosophical Transaction A, The Royal Society, Vol. 372-2022, Article ID:20130325, 2014.
  • 4. Abe, Y., Nonomura, T., Iizuka, N. and Fujii, K., “Geometric interpretations and spatial symmetry property of metrics in the conservative form for high-order finite-difference schemes on moving and deforming grids,” Journal of Computational Physics, Vol.260, pp.163-203 2014.
  • 5. Kondo, K., Aono, H., Nonomura, T., Anyoji, M., Liu, T., Oyama, A., Fujii, K. and M. Yamamoto, “Analysis of owl-like airfoil aerodynamics at low Reynolds number flow,” Transactions of JSASS Space Technology Japan 2014.
  • 6. Anyoji, M., Okamoto, M., H. Hidaka, Kondo, K., Oyama, A., H. Nagai and Fujii, K., “Control surface effectiveness of low Reynolds number flight vehicles,” Journal of Fluid Science and Technology, Vol. 9, No.5, paper No. 14-00176, 2014.
  • 7. Anyoji, M., Okamoto, M., Hidaka, H., Nonomura, T., Oyama, A. and Fujii, K., “Planetary atmosphere wind tunnel tests on aerodynamic characteristics of a mars airplane scale model,” Transactions of JSASS Space Technology Japan Vol. 12, No. ISTS29, pp. Pk_7-Pk-12 2014．
  • 8. T. Nonomura, S. Morizawa, S. Obayashi and K. Fujii, “Computational Prediction of Acoustic Waves from a Subscale Rocket Motor”, JSASS, Transaction of JSASS, Aerospace Technology Japan, Vol.12, No ists29, pp.11-17, May 2014.
  • + 3 journal articles in Japanese

2013

  • 1. Aono, H., Nonomura, T., Iizuka, N., Ohsako, T., Inari, T., Hashimoto, Y., Takaki, R. and Fujii, K., “Scalar tuning of a fluid solver using compact scheme for a supercomputer with a distributed memory architecture,” CFD letters, Vol. 5(4), pp.143-152, 2013.
  • 2. Y.Nagata, T. Nonomura, K.Fujii and M.Yamamoto, “Analysis of Acoustic-fields Generated by a Supersonic Jet Impinging on Flat and Curved Inclined Plates”, International Journal of Aerospace and Lightweight Structures, Vol.3, No.3, November 2013 DOI: 10.3850/S2010428613000068
  • 3. T. Nonomura, K. Kitamura and K. Fujii, “A simple interface sharpening technique with a hyperbolic tangent function applied to compressible two-fluid modeling,” Journal of Computational Physics, Elsevier, Vol. 258, pp.95-117, February 2014.
  • 4. Li, W., Nonomura, T., and Fujii, K., “Mechanism of controlling supersonic cavity oscillations using upstream mass injection,” Physics of Fluids, Vol. 25, 086101, 2013.
  • 5. Liu, T., Oyama, A. and Fujii, K., “Scaling Analysis of Propeller-Driven Aircraft for Mars Exploration,” Journal of Aircraft Vol. 50, No. 5, pp. 1593-1604, doi: 10.2514/1.C032086, 2013
  • 6. Li, W., Nonomura, T. and Fujii, K., “On the Feedback Mechanism in Supersonic Cavity Flows,” Physics of Fluids, Vol. 25, pp. 056101, May 2013.
  • 7. Nonomura, T., Fukumoto, H., Ishikawa, Y. and Fujii, K., “Mach Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings”, AIAA Journal, Vol.51, No. 9, pp. 2281-2286, September, 2013.
  • 8. Nonomura, T. and Fujii, K., “Robust Explicit Formulation of Weighted Compact Nonlinear Scheme,” Computers & Fluids, Vol. 85(1), pp.8-18 2013
  • + 3 journal articles in Japanese

2012

  • 1. Kojima, R., Nonomura, T., Oyama, A. and Fujii, K., “Large-Eddy Simulation of Low-Reynolds- Number Flow Over Thick and Thin NACA Airfoils,” Journal of Aircraft, Vol.50, No.1, PP187-196, January 2013.
  • 2. Okada, K., Nonomura, T., Fujii, K. and Miyaji, K., “Computational Analysis of Vortex Structures Induced by a Synthetic Jet to Control Separated Flows,” International Journal of Flow Control, Vol. 4, No.1+2・2012, pp 45-46, January 2013.
  • 3. Abe, Y., Iizuka, N., Nonomura, T., and Fujii, K., “Conservative metric Evaluation for high-order finite difference schemes with the GCL identities on moving and deforming grids,” Journal of Computational Physics, Vol. 232, pp.14-21, January 2013.
  • 4. Li, W., Nonomura, T., Oyama. A. and Fujii, K., “Feedback Mechanism in Supersonic Laminar Cavity Flows,” AIAA Journal, Vol.51, No.1, pp. 253-257, January 2013.
  • 5. Inaba, R., Nishida, H., Nonomura, T., Asada, K. and Fujii, K., “Numerical Investigation of Asymmetric Separation Vortices over Slender Body by RANS/LES Hybrid Simulation,” Transactions of The Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 10(2012) No. ISTS28, pp. Pe_89_96, 2012.
  • 6. Tatsukawa, T., Nonomura, T., Oyama, A. and Fujii, K., “Aerodynamic Design Exploration for Reusable Launch Vehicle using Genetic Algorithm with Navier Stokes Solver”, Transactions of The Japan society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 10, No.ists28, pp.55-63, 30 August 2012.
  • 7. Kaneda, I., Sekimoto. S., Nonomura. T., Asada. K., Oyama. A. and Fujii, K., “An Effective Three-Dimensional Layout of Actuation Body Force for Separation Control,” International Journal of Aerospace Engineering, Vol. 2012(2012), Article ID 786960, May 2012.
  • 8. Nonomura, T., Morizawa, S., Terashima, H., Obayashi, S and Fujii, K., “ Numerical (error) issues on compressible multicomponent flows using a high-order differencing scheme: Weighted compact nonlinear scheme,” Journal of Computational Physics, Vol. 231, No. 8, pp. 3181-3210, 2012.
  • 9. Okada, K., Oyama, A., Fujii, K. and Miyaji, K., “Computational Study of Effects of Non-dimensional Parameters on Synthetic Jets,” Transactions of the Japan Society For Aeronautical And Space Sciences, Vol. 55, No. 1 pp. 1-11, 2012.
  • + 1 journal articles in Japanese

2011

  • 1. Nonomura, T. and Fujii, K., “Overexpansion Effects on Characteristics of Mach Waves　from a Supersonic Cold Jet,” AIAA Journal, Vol. 49, No. 10, 2011.
  • 2. Nonomura. T. and Fujii. K., “Recent Efforts in Rocket Plume Acoustics” CFD Review2010, World Scientific, pp.421-446, July 2011.
  • 3. Nonomura, T., Goto, Y. and Fujii, K., “Aero-acoustic waves generated from a supersonic jet impinging on an inclined flat plate,” aero-acoustics International Journal of Aero-acoustics, Vol. 10, No. 4, pp. 401 – 426, 2011.
  • 4. Nonomura, T., Li, W., Goto, Y. and Fujii, K., “Efficiency Improvements of Seventh-order Weighted Compact Nonlinear Scheme,” Computational Fluid Dynamics Journal, Vol.18, No, 2, pp. 180-186, 2011.
  • + 1 journal articles in Japanese

2010

  • 1. Fujii, K., Nonomura., T and Tsutsumi., S, “Toward Accurate Simulation and Analysis of Strong Acoustic Wave Phenomena—A review from the Experience of Our Study on Rocket Problems,” International Journal for Numerical Methods in Fluids, Vol.64, pp.1412-1432, December 2010.
  • 2. Oyama, A., Nonomura, T. and Fujii, K., “Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition,” Journal of Aircraft, Vol. 47, No. 5, pp. 1756-1762, 2010.
  • 3. Okada, K., Oyama, A., Fujii, K. and Miyaji, K., “Computational Study on Effect of Synthetic Jet Design Parameters,” International Journal of Aerospace Engineering, Vol. 2010, Article ID 364859, 2010．
  • 4. Nonomura, T., Iizuka, N. and Fujii, K., “Free-stream and vortex preservation properties of high-order WENO and WCNS on curvilinear grids,” Computers & Fluids 39, pp. 197–214, 2010.
  • 5. Nonomura, T., Muranaka, H. and Fujii, k., “Computational Analysis of Mach Number Effects on the Edgetone Phenomenon,” AIAA Journal, Vol. 48, No. 6, 2010.
  • + 3 journal articles in Japanese

2009以前-

  • 1. Nonomura, T., Muranaka, H. and Fujii, K., “Computational Analysis of the Characteristics of High-Speed Flows over a Delta Wing,” Computational Fluid Dynamics (CFD) Journal, Vol. 17, No. 4, pp. 267-274, October 2009.
  • 2. Oyama, A., Okabe, Y., Shimoyama K. and Fujii, K., “Aerodynamic Multi-objective Design Exploration of a Flapping Airfoil Using a Navier-Stokes Solver,” Journal of Aerospace Computing, Information, and Communication, AIAA online, DOI:10.2514/1.35992, 2009.
  • 3. Nonomura, T. and Fujii, K., “Effects of Difference Scheme Type in High-order Weighted Compact Nonlinear Schemes,” Journal of Computational Physics, Vol. 228, pp. 3533-3539, 2009.
  • 4. Fujii, K., Imai, G. and Ogawa, A., “Computational analysis of the characteristics of high-speed flows over a delta wing,” Computational Fluid Dynamics Journal, 2008.
  • 5. Fujii, K., “CFD Contributions to Shock-related Problems,” Shock Waves, No.2008, Vol. 18, pp.145-154, 2008.
  • 6. Shimoyama, K., Oyama A., and Fujii, K., “Development of Multi-Objective Six-Sigma Approach for Robust Design Optimization,” Journal of Aerospace Computing, Information, and Communication, Vol. 5, Online Journal, 2008.
  • 7. Kawai S., and Fujii, K., “Compact Scheme with Filtering for Large-Eddy Simulation of Transitional Boundary Layer”, AIAA Journal, Vol.46, No.3, pp.690-700, 2008.
  • 8. Oyama, A., Shimoyama, K. and Fujii, K., “New Constraint-Handling Method for Multi-Objective and Multi-Constraint Evolutionary Optimization,” Transactions of JSASS, Vol. 50, No. 167, pp. 56-62, 2007．
  • 9. Kawai, S. and Fujii, K., “Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows,” AIAA Journal, Vol. 45, No. 1, pp. 289-301, 2007.
  • 10. Terashima, H. and Fujii, K., “Influence of Stores on the Transonic Flutter of a Delta Wing Configuration,” AIAA Journal, Vol. 45, No. 1, pp. 237-246, 2007.
  • 11. Nakai, Y., Fujimatsu, N. and Fujii, K., “Experimental Study of Underexpanded Supersonic Jet Impingement on an Inclined Flat Plate” AIAA Journal, Vol. 44, No. 11, pp. 2691-2699, 2006.
  • 12. Fujimoto, K. and Fujii, K., “Computational Aerodynamic Analysis of Capsule Configurations toward the Development of Reusable Rockets,” Journal of Spacecraft and Rockets, Vol. 43, No. 1, pp. 77-83, 2006.
  • 13. Fujii, K., “Some Remarks on the CFD Research for Space Transportation System Development,” Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 90, pp. 3
  • 14. Fujii, K., “Progress and Future Prospects of CFD in Aerospace –Wind Tunnel and Beyond,” Progress in Aerospace Sciences, Vol. 41, No. 6, pp. 455-470, Elsevier, 2005.
  • 15. Fujimatu, N., Tamura, Y. and Fujii, K., “Improvement of Noise Filtering and Image Registration Methods for the Pressure Sensitive Paint Experiments,” Journal of Visualization, Vol. 8, No. 3, pp. 225-233, 2005.
  • 16. Kawai, S. and Fujii, K., “Computational Study of Supersonic Base Flow Using Hybrid Turbulence Methodology,” AIAA Journal, Vol. 43, No. 6, pp. 1265-1275, 2005.
  • 17. Kawai, S. and Fujii, K., “Analysis and Prediction of Thin-Airfoil Stall Phenomena with Hybrid Turbulence Methodology,” AIAA Journal, Vol. 43, No. 5, 2005.
  • 18. Fujimoto, K. and Fujii, K., “Assessment of CFD Estimation of Aerodynamic Characteristics of Basic Reusable Rocket Configurations”, Transaction of the Japan Society for Aeronautical and Space Sciences, Vol. 48. No. 159, pp. 13-20, May 2005.
  • 19. Fujii, K., “Some Remarks on the ulations for the Fluid Dynamic Research for Space Transportation Systems,” Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 90, Springer, 2005.
  • 20. Arasawa, T., Fujii, K., and Miyaji, K., “High-order Compact Difference Scheme Applied to Double-Wing Vortical Flows,” Journal of Aircraft, Vol. 41, No. 4, pp. 953-957, 2004.
  • 21. Ito, T. and Fujii, K., ”Flow Field and Performance Analysis of the Aerospike Nozzles with Simplified Clustered Modules,” Transaction of the Japan Society for Aeronautical and Space Sciences, Vol. 47, No. 155, pp.17-22, 2004.
  • 22. Ito, T. and Fujii, K., ” Flow Field and Performance Analysis of an Annular-Type Aerospike Nozzle with Base Bleeding, Transaction of the Japan Society for Aeronautical and Space Sciences Vol. 46, No. 151, pp.17-23, May 2003
  • 23. Teramoto, S. and Fujii, K., “Mechanism of Dynamic Instability of a Reentry Capsule at Transonic Speeds,” AIAA Journal, Vol. 40, No. 12, pp. 2467-2475, 2002.
  • 24. Fujii, K., Imai, K. and Sato, T., “Computational Analysis of the Flow Field Near the Boat-tail Region of Annular Plug Nozzles,” JSME International Journal, Series B, Vol. 45, No.4, 2002.
  • 25. Fujii, K., Tsuboi, N. and Fujimatsu, N., “Visualization of Jet Flows over a Plate by Pressure –Sensitive Paint Experiments and Comparison with CFD,” Visualization and Imaging in Transport Phenomena, Vol. 972, pp. 265-270, Annals of The New York Academy of Sciences, 2002.
  • 26. Ito T. and Fujii, K.. “Numerical Investigations of the Base-Flow Characteristics of Axisymmetric Aerospike Nozzles,” Transaction of the Japan Society for Aeronautical and Space Sciences, Vol. 45, No. 148, 2002.
  • 27. Terashima, H. and Fujii, K., “Time Accuracy of the Transonic Viscous Flow Calculations for the Oscillating Wings,” Computational Fluid Dynamics Journal, Vol.11, No.2, p.225-233, 2002.
  • 28. Ito, T., Fujii, K., and Hayashi, K., “Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structures and Thrust Performance,” Journal of Propulsion and Power, Vol. 18, No. 2, pp. 254-260, 2002.
  • 29. Fujii, K., “Lessons Learned from the blast Wave Computation Using Overset Moving Grids.-Grid Motion Improves the Resolution-,” Innovative Methods for Numerical Solutions of Partial Differential Equations, World Scientific, 2002.
  • 30. Fujii, K., “CFD Applications to Space Transportation Systems,” Frontiers of Computational Fluid Dynamics (book) 2002.
  • 31. Fujii, K., “Real-time Computation and Visualization on Mobile PC’s,” Computational Fluid Dynamics for the 21st Century, 2001.
  • 32. Teramoto, S. and Hiraki, K. and Fujii, K., “Numerical Analysis of Dynamic Stability of a Reentry Capsule at Transonic Speeds,” AIAA Journal, Vol. 39, No. 4, pp.646-653, 2001.
  • 33. Teramoto, S. and Fujii, K., “Preprocessed Visualization of Large Scale Unsteady Flow Simulations,” Journal of Visualization, Vol. 3, No. 4, pp. 313-321, 2001.
  • 34. Fujii, K., “Role of CFD for the Fluid Dynamic Education,” Computational Fluid Dynamics Journal, Vol. 9, No. 3, pp. 194-199, 2000.
  • 35. Fujii, K., “Efficiency Improvement of Unified Implicit Relaxation/Time Integration Algorithms,” AIAA Journal, Vol. 37, No. 1, pp.125-128, 1999.
  • 36. Fujii, K. and Ogawa, T., “What Have We Learned from CFD Research on Train Aerodynamics,” Frontiers of Computational Fluid Dynamics, 1998.
  • 37. Fujii, K., and Shimizu, F., “Computation of Blast Wave Propagation Using an Overset Moving Zonal Method,” CFD Review1998, World Scientific, 1998.
  • 38. Matsuo, A. and Fujii, K., “Prediction Method of Unsteady Combustion around Hypersonic Projectile in Stoichiometric Hydrogen-Air,” AIAA Journal, Vol. 36, No. 10, pp. 1834-1841, 1998.
  • 39. Watanabe, R., Fujii, K., and Higashino, F., “Three-Dimensional Flow Computation Around a Projectile Overtaking a Preceding Shock Wave,” Journal of Spacecraft and Rockets, Vol. 35, No. 5, pp. 619-625, 1998.
  • 40. Watanabe, R., Fujii, K., and Higashino, F., “Computational Analysis of the Unsteady Flow Induced by a Projectile Overtaking a Preceding Shock Wave,” Transaction of the Japan Society for Aeronautical and Space Sciences, Vol. 41, No. 132, pp. 65-73, 1998.
  • 41. Matsuo, A. and Fujii, K., “Numerical Investigation of the One-dimensional Piston Supported Detonation Waves,” Energy Conversion and Management, Vol. 38, No. 10-13, pp. 1283-1295, 1997.
  • 42. Fujii, K. and Tamura, Y., “Effect of Engine Integration on the Aerodynamic Characteristics of a Spaceplane,” International Journal of Computational Fluid Dynamics, Vol. 8, No. 4, pp.235-246, 1997.
  • 43. Ogawa, T. and Fujii, K., “Numerical Investigation of Three Dimensional Compressible Flows Induced by a Train Moving into a Tunnel,” Computers & Fluids, Vol. 26, pp. 565-585, 1997.
  • 44. Matsuo, A. and Fujii, K., “Detailed Mechanism of the Unsteady Combustion around Hypersonic Projectile,” AIAA Journal, Vol. 34, No. 10, pp. 2082-2089, 1996.
  • 45. Miyaji, K. and Fujii, K., and Karashima, K., “Enhancement of the Leading-Edge Separation Vortices by the Trailing-Edge Lateral Blowing,” AIAA Journal, Vol. 34, No. 9, 1996.
  • 46. Fujii, K., “Performance of a Japanese Vector-Parallel Supercomputers on Large-Scale CFD Problems,” Solution Techniques for Large-Scale CFD Problems, Computational Methods in Applied Sciences, pp.123-137, 1995.
  • 47. Matsuo, A. and Fujii, K., “Computational Study of Large-Disturbance Oscillations in Unsteady Supersonic Combustion around Projectiles,” AIAA Journal, Vol. 33, No. 10, pp. 1828-1835, 1995.
  • 48. Fujii, K., and Ogawa, T., “Aerodynamics of High Speed Trains Passing by Each Other,” Computers & Fluids, Vol. 24, 1995.
  • 49. Matsuo, A., Fujii, K., and Fujiwara, T., “Flow Features of Shock-Induced Combustion around Projectile Traveling at Hypervelocities,” AIAA Journal, Vol. 33, No 6, pp 1056-1063, 1995.
  • 50. Fujii, K., “Unified Zonal Method Based on the Fortified Solution Algorithm”, Journal of Computational Physics, Vol. 118, pp. 92-108, 1995.
  • 51. Yamauchi, M., Fujii, K., and Higashino, F., “Numerical Investigation of Supersonic Flows around a Spiked Blunt-Body,” Journal of Spacecraft and Rockets, Vol. 32, No. 1, 1994.
  • 52. Tamura, Y. and Fujii, K., “Simulation of Experimental Visualization Methods for Computational Fluid Dynamics Research,” International Journal of Computational Fluid Dynamics, Vol. 2, 1994.
  • 53. Ogawa, T. and Fujii, K., “Numerical Simulation of Compressible Flows Induced by a Train Moving into a Tunnel,” Computational Fluid Dynamics Journal, Vol. 3, No. 1, 1994.
  • 54. Dindar, M., Kaynak, U. and Fujii, K., “Non-equilibrium Turbulence Modeling Study on Light Dynamic Stall of a NACA 0012 Airfoil,” Journal of Aircraft, Vol. 30, 1993.
  • 55. Shimizu, F. Fujii, K., and Higashino, F., “Ground Surface Effect on the Blast Wave Propagation in Two Dimensions,” Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 36, No.111, 1993.
  • 56. Fujii, K., and Yoshihara H., “Navier-Stokes Benchmark Tests” Supercomputers and Their Performance in Computational Fluid Dynamics, Notes on Numerical Fluid Mechanics, Vol. 37, pp. 105-126, Vieweg, 1993.
  • 57. Tamura, Y. and Fujii, K., “A Multi-Dimensional Upwind Scheme for the Euler Equations on Structured Grids,” Computers & Fluids, Vol. 22, No. 2-3, 1993.
  • 58. Fujii, K., and Tamura, Y., “Recent Applications of the FNS Zonal Method to Complex Flow Problems,” SAE 1992 AEROSPACE Transaction Vol. 100, Journal of Aerospace, Section 1, Part 2, SAE International, 1992.
  • 59. Fujii, K., Endo, H. and Yasuhara, M., “Activities of Computational Fluid Dynamics in Japan: Compressible Flow Simulations,” High Performance Computing Research and Practice in Japan, Wiley Professional Computing, pp. 139-161, John Wiley and Sons, 1990.
  • 60. Nagasu, H. and Fujii, K., “Navier-Stokes Code Development for Transonic Flow Simulations,” Computational Methods in Viscous Aerodynamics, Elsevier, pp. 273-300, 1990.
  • 61. Fujii, K., “Supercomputers and Graphic Workstations in Fluid Dynamics Research,” Visualization in Supercomputing, Springer, pp. 3-14, 1990.
  • 62. Fujii, K. and Obayashi, S., “High-Resolution Upwind Scheme for Vortical-Flow Simulations,” Journal of Aircraft, Vol. 26, No. 12, pp. 1123-1129, 1989.
  • 63. Fujii, K. and Lewis, B. Schiff, “Numerical Simulations of Vortical Flows over a Strake-Delta Wing,” AIAA Journal, Vol. 27, No. 9, pp. 1153-1162, 1989.
  • 64. Fujii, K., Sharad G., and Terry L. Holst, “Evaluation of Navier-Stokes and Euler Solutions for Leading Edge Separation Vortices,” International Journal of Numerical Methods in Fluids, Vol. 8, No. 10, pp. 1319-1329, 1988.
  • 65. Fujii, K. and Obayashi, S., “Navier-Stokes Simulations of Transonic Flows over a Wing Fuselage Combination,” AIAA Journal, Vol. 25, No. 12,1987.
  • 66. Fujii, K. and Obayashi, S., “Navier-Stokes Simulations of Transonic Flows over a Practical Wing Configuration,” AIAA Journal, Vol. 25, No. 3, pp. 369-370, 1987.
  • 67. Fujii, K. and Karashima, K., “Second-Order Transonic Small Perturbation Flow,” Transactions of the Japan Society for Aeronautics & Space Sciences, Vol. 21, No. 51, pp. 24-34, 1978.
  • + 52 journal articles in Japanese