成果論文

2021 | 2020 | 2019 | 2018 |2017 |2016 |2015 | 2014 | 2013 | 2012 | 2011 | 2010 | 2009以前- |     

2021

  • 1. K. Sekine, T. Tatsukawa, K. Fujii and E. Itoh, “Multi-objective takeoff time optimization using cellular automaton-based simulator”, IEEE Access, 2021, ; DOI: https://doi.org/10.1109/ACCESS.2021.3084215
  • 2. 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; https://doi.org/10.1121/10.0005313
  • 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. 藤井孝藏, “計算工学の視点でみる「ものづくり」デジタルツイン構築への道”, 計算工学,Vol. 26, No. 2, pp. 3-8, 2021
  • 5. 立川智章,関根將弘,藤井孝藏,伊藤恵理,都築怜理,柳澤大地,西成活裕,安福建祐,“全体最適のための新たな航空交通モデルの開発”,計算工学,Vol. 26,No.3,pp. 19-22,2021
  • 6. 立川智章,小川拓人,浅田健吾,藤井孝藏,“非定常流れ場の分析に向けた簡易渦構造同定手法”,可視化情報,Vol.41,No.162,pp.25-26,2021年10月

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, Jan. 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 Airfoil”, AIAA Journal, Vol. 58, No. 10, pp. 4243–4259, Oct. 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.
  • 6. 八木楓,山口鳳太,赤松浩,関本諭志,藤井孝藏,“無人航空機への搭載を目的としたプラズマアクチュエータ用の小型ナノ秒パルス高電圧電源の開発”,プラズマ応用科学,Vol. 28, No. 2,pp. 11-16,Dec. 2020.
  • 7. 関本諭志,藤井孝藏, “模型飛行機へのプラズマアクチュエータの適用と関連要素研究”, 日本流体力学会誌「ながれ」,Vol. 39,No.4,pp. 222-229, August 2020.

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
  • 6. 西田浩之,下村怜,関本諭志,大山聖,藤井孝藏,“能動的流体制御デバイスを用いた翼周り剝離流れ制御への深層強化学習の応用”,日本流体力学会誌「ながれ」,Vol. 38, No.5,pp. 323-328, Oct. 2019.
  • 7. 長岡慎介,立川智章,藤井孝藏,“ステップバック・セルオートマトンを用いた航空交通シミュレーション”,HPCI利用研究成果集,Oct. 2019.
  • 8. 藤井孝藏,浅田健吾,“低レイノルズ数流れに対するCFD研究の現状と将来”,日本航空宇宙学会誌, Vol. 67, No. 5, pp. 174-180, May 2019 ; https://doi.org/10.14822/kjsass.67.5_174.

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
  • 6. 藤井孝藏,プラズマアクチュエータ:大規模流れ制御の可能性を拓く小型デバイス,日本流体力学会誌「ながれ」,Vol. 36, pp. 349-358, 2017.
  • 7. 田村善昭,大林茂,梶島岳夫,島英志,中橋和博,姫野龍太郎,藤井孝藏,古川雅人,山本誠,特別企画:数値流体力学シンポジウムの 30年 ~できたこと,できなかったこと~,日本流体力学会誌「ながれ」,Vol. 36, pp. 61-68, 2017.

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, 2016DOI: 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
  • 15. 焼野藍子,河合宗司,野々村拓,藤井孝藏,“二次元ハンプ剥離後流渦への周期的制御振動周波数の影響,”ながれ,Vol. 34, pp. 97-102, 2015.
  • 16. 深潟康二,青野光,藤井孝藏,山田俊輔,石川仁,松野隆 “プラズマアクチュエータの動向―基礎的な流れ場に対する実験的・数値的研究―” プラズマ核融合学会誌第91巻10号p657-660 2015.
  • 17. 松野隆,本阿弥眞治,藤井孝藏,関本諭志,飯田明由 “ プラズマアクチュエータの動向―流体計測法― ” プラズマ核融合学会誌第91巻10号p661-664 2015.
  • 18. 藤井孝藏,野々村拓,青野光,佐藤允,焼野藍子 “流体制御を利用した輸送システム・流体機器設計概念の革新を目指して ―「京」利用による流れ現象理解と制御パラメータの発見” 計算工学会Vol20.No4. 2015.

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.
  • 9. 藤井孝藏, “学術論文誌のあり方 -日本機械学会における学術論文誌の再編から-,” 科学技術振興機構, 情報管理, Vol.57, no.8, November 2014.
  • 10. 藤井孝藏,野々村拓,青野光,佐藤允,焼野藍子 “ 革新的流体制御技術の研究開発「京」大規模計算によるマイクロデバイス ” ターボ機械,May 2014.
  • 11. 大山聖,立川智章,野々村拓,藤井孝藏,“空力音響多目的設計探査-ロケット射点形状設計への適用-”,ターボ機械, Vol. 42, No.5, pp.305-309, May 2014.

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
  • 9. 大山聖,岡田浩一,浅田健吾,野々村拓,宮路幸二,藤井孝藏, “シンセティックジェットによる流れの能動制御,” 日本航空宇宙学会誌, Vol. 61(2), pp. 57-63, 2013.
  • 10. 浅田健吾, 河合宗司, 藤井孝藏, “LESのダイナミック壁面モデル:剥離・遷移・再付着を伴う高レイノルズ数翼流れ”, ながれ, Vol.32, pp.95-105, 2013.
  • 11. 佐藤允, 岡田浩一, 青野光, 焼野藍子, 野々村拓, 藤井孝藏, “ DBDプラズマアクチュエータを用いた翼剥離制御の大規模パラメトリックス”, ながれ, Vol.32, pp.145-148, 2013.

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.
  • 10. 立川智章,大山聖,藤井孝藏, “GPを用いた非劣解からの設計情報の抽出,” 進化計算学会論文誌, Vol. 3 (3), pp. 133-142, 2012.

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.
  • 5. 藤井孝藏, “HPCIコンソーシアムについて -次世代スパコン利用に関する最近の動き-” ながれ, Vol.30, No.2, pp.55-57, 2011.

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.
  • 6. 滑 慶則,高木 亮治,大山 聖,藤井 孝藏,山本 誠, “再使用観測ロケット空力形状に関する設計探査”, 日本機械学会論文集 C編 第76巻 第771号 pp. 2811-2818, 2010.
  • 7. 藤井孝藏, 浅田健吾, “DBDプラズマアクチュエータによる翼剥離制御メカニズム−バースト波解析が語るもの−,” ながれ Vol. 29, No. 4, pp. 303-309, 2010.
  • 8. 堤誠司,福田紘大,高木亮治,嶋英志,藤井孝藏, “ロケット打上げ時の音響振動について”, 騒音制御, Vol.34, No.4, pp. 303-309, 2010.

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.
  • 68. 久保田 孝,尾川 順子,藤田 和央,大山 聖,藤井 孝蔵, “MELOSのミッション検討と工学的チャレンジ,” 日本惑星科学会誌 遊星人, Vol.18, No.2, 2009.
  • 69. 野々村拓, 村中洋子, 藤井孝藏, “エッジトーンの数値解析における境界条件の影響,” Transaction of JSCES No. 20080030, Online Journal, 2008.
  • 70. 野々村拓, 村中洋子, 藤井孝藏, “エッジトーンの擾乱伝播速度の解析,” Transaction of JSCES No. 20080022, Online Journal, 2008.
  • 71. 大山聖, 藤本圭一郎, 飯塚宣行, 角有司, 川添通宏, 高木亮治, 藤井孝藏, 沖田耕一, “JAXA基幹ロケットの信頼性向上へ向けたバルブ開発プロセス革新への取り組み,” 設計工学, 第43巻第4号, pp203-210, 平成20年4月(2008).
  • 72. 藤井孝藏, “ペタスケールコンピューティング ー航空宇宙分野からの期待,” 計算工学, Vol. 13, No.1, pp.1740-1745, 2008.
  • 73. 藤井孝藏, 松野隆, “DBDプラズマアクチュエータ−バリア放電を利用した新しい流体制御技術−,” 機械学会流体工学部門ニュースレター−流れ, 2007年12月号(ウェブ解説)2008.
  • 74. 椿野大輔, 田中義輝, 藤井孝藏,”プラズマアクチュエータを用いた翼前縁剥離の制御における位置及び個数の影響,”日本機械学会論文集B編, 第73巻727号, pp. 663-669, 2007.
  • 75. 佐宗章弘,藤井孝藏,矢部孝,”局時によって流れを変える,”日本機械学会論文集B編, 第73巻727号, pp. 650-654, 2007.
  • 76. 藤井孝藏, “流体シミュレーション:過去, 現在, 未来,” 計算工学, 計算工学会学会誌, Vol. 11, No. 1 , 2006, pp. 10-15, 2006.
  • 77. 藤井孝藏, 中井祐輔, 藤松信義, 大内弘文, “感圧塗料PSP:空力現象解明の道具として,” 日本航空宇宙学会誌, 「特集感圧塗料」, Vol. 54, No. 624, 2006.
  • 78. 寺島洋史, 藤井孝藏, “遷音速フラッターシミュレーションにおける陰解法の時間刻み幅選定基準について,” 日本機械学会論文集B編, Vol. 71, No. 712, pp.2856-2863, 2005.
  • 79. 村中洋子, 野々村拓, 藤井孝藏, “エッジトーン周波数特性の数と数値のシミュレーション,” Transaction of JSCES No. 20050026, Online Journal, 2005.
  • 80. 藤井孝藏, “CFDに関わる可視化技術-昔話と今後への期待,” 可視化情報学会誌,Vol. 25, No.98 , pp. 39-44, 2005.
  • 81. 大山聖, 藤井孝藏,”JAXA/ISASにおけるロケット・宇宙機研究開発へのCFDの活用,” 日本流体力学会誌「ながれ」, Vol. 24, No. 3, pp.289-296, 2005.
  • 82. 藤井孝藏, “航空宇宙におけるCFD,” 日本流体力学会誌「ながれ」, 8月号, Vol. 23, No.4, pp.233-241, 2004.
  • 83. 藤井孝藏, “CFD研究を再考するー航空宇宙工学として,” 日本航空宇宙学会誌, 「特集CFDの最前線」, Vol. 51, No. 599, pp306-312, 2003.
  • 84. 藤井孝藏, “変わりゆく流体シミュレーション技術,” 土木学会誌,特集「計算力学の最前線」,Vol. 88, pp.12-14, 2003.
  • 85. 藤井孝藏, “第6回野辺山国際CFDワークショップ,” 計算工学誌「計算工学」, シンポジウム報告書, Vol. 8, No. 3, 2003.
  • 86. 藤井孝藏, “CFD思い出話—航空宇宙関連を中心に,” 日本数値流体力学会誌(最終号), WEB Journal , 第10巻第3号, PP. 237-240, 2002.
  • 87. 市川治, 藤井孝藏, “直交格子を使用した3次元の任意形状物体まわりの流体シミュレーション,” 日本機械学会論文集B編, Vol. 69, No. 669, pp.1329-1336, 2002.
  • 88. 藤井孝藏, “CFDの新展開—曲がり角に来たCFD技術とその利用” 日本流体力学会誌「ながれ」,Vol. 21, No.1, pp.46-54, 2002.
  • 89. 小川隆申, 藤井孝藏, “高速列車トンネル突入による低周波音問題—航空 宇宙技術の利用による現象解明と対策,” 日本航空宇宙学会誌 Vol. 49, No. 571, pp.170-175, 2001. 
  • 90. 藤井孝藏, “数値シミュレーションが開く世界−数値実験は物理実験を越えられるか?,” 日本電子情報通信学会,Vol.84, No.6, pp.375-378, 2001.
  • 91. 藤井孝藏, “世紀末夏のCFD国際会議(※学術講演会報告),” 日本計算工学会誌「計算工学」,Vol.6, No.1, pp. 245-246, 2001.
  • 92. 藤井孝藏, “パネルディスカッション「流体実験の現在」−それから,” 日本数値流体力学誌「数値流体力学」,Vol. 8,No. 3,pp.105-107, 2000.
  • 93. 藤井孝藏, “有限体積法の最前線−高速気流計算法の最近の動向,” 日本計算工学会誌「計算工学」, Vol. 3, No. 3, pp. 158-166, 1998.
  • 94. 藤井孝藏, “計算結果の可視化技術 特集(熱流体の数値計算),” 日本ガスタービン学会誌, Vol. 26, No. 102, pp. 25-29, 1998.
  • 95. 坂本和之, 藤井孝藏, 田村善昭, 松永康二, “超音速内部流路における3次元キャビティー流れの数値解析,” 日本機械学会論文集B編, Vol. 63, No. 606, pp. 491-496, 1997.
  • 96. 藤井孝藏, “サイエンティフィック・ビジュアライゼーション第3回現状と将来,” 日本計算工学会誌「計算工学」, Vol. 1, No. 3, pp.48-52, 1996.
  • 97. 小川隆申, 藤井孝藏, “微気圧波軽減のための理論的列車先頭形状設計法,” 日本機械学会論文集B編, Vol. 62, No.599, pp. 139-146, 1996.
  • 98. 藤井孝藏, “サイエンティフィックビジュアライゼーション,第2回 画像表示作業の実際,” 日本計算工学会誌「計算工学」, Vol. 1, No. 2, pp.85-92, 1996.
  • 99. 藤井孝藏, “CFDにおける可視化処理,” 日本航空宇宙学会誌, Vol. 44, No. 509, pp. 379-385, 1996.
  • 100. 藤井孝藏, “サイエンティフィックビジュアライゼーション,第1回 可視化の基礎,” 日本計算工学会誌「計算工学」, Vol. 1, No. 1, pp. 26-29, 1996.
  • 101. 坂本和之, 藤井孝藏, 田村善昭, 松永康二, “超音速内部流路におけるキャビティーまわりの流れ特性,” 日本機械学会論文集B編, Vol. 62, No. l 595, pp. 139-146, 1996.
  • 102. 渡辺力夫, 藤井孝藏, 東野文男, “トンネル内圧縮波の一次元数値シミュレーション,” 日本機械学会論文集B編, Vol. 61, No. 592, 1995.
  • 103. 田村善昭, 藤井孝藏, “ 数値流体力学における可視化(Ⅳ)ハードウェアと可視化の将来,” 日本数値流体力学会誌, Vol. 3, No. 3, pp. 228-240, 1995.
  • 104. 小川隆申, 藤井孝藏, “定常流を用いた列車トンネル突入時の圧縮波面勾配予測法,”日本機械学会論文集B編, Vol. 61, No. 586, pp. 170-176, 1995.
  • 105. 藤井孝藏, “研究所紹介「宇宙科学研究所」,”日本可視化情報学会誌, Vol. 15, No. 57, pp. 56-59, 平成7年4月 (1995).
  • 106. 藤井孝藏, “CFDの最近の進歩と将来展望(1)--圧縮性流れの数値計算法—,”ターボ機械, Vol. 23, No. 3, pp. 128-132,1994.
  • 107. 田村善昭, 藤井孝藏, “数値流体力学における可視化(Ⅲ)可視化手法の詳細” 日本数値流体力学学会誌, Vo3. , No. 1,1994.
  • 108. 田村善昭, 藤井孝藏, “数値流体力学における可視化(Ⅱ)ソフトウェアの準備”日本数値流体力学学会誌,Vol. 2, No. 4, 1994.
  • 109. 田村善昭, 藤井孝藏, “数値流体力学における可視化(Ⅰ)可視化入門,” 日本数値流体力学学会誌, Vol. 2, No. 3, 1994
  • 110. 藤井孝藏, “航空宇宙工学におけるスーパーコンピューティング,” 情報処理(情報処理学会誌)Vol. 36, No. 2, pp. 154-158, 1994.
  • 111. 藤井孝藏, “数値流体力学における可視化(Ⅰ)可視化入門,” 機械の研究, Vol. 45, No.1, 平成5年1月, 1993.
  • 112. 藤井孝藏, “宇宙輸送に関わる流体解析,” 機械の研究, Vol. 45, No. 1, 1993.
  • 113. 藤井孝藏, “スポーツ工学のすすめ,” シミュレーション(日本シミュレーション学会誌), 平成4年9月, Vol. 11, No.3, (1992).
  • 114. 藤井孝藏, 田村善昭, “高速気流の数値シミュレーションと可視化,” 可視化情報, Vol. 11, No.41, 平成3年4月(1991).
  • 115. 藤井孝藏, “数値流体力学:最近の成果と動向,” 日本航空宇宙学会誌, Vol. 37, No. 421, pp. 82-90, 1988.
  • 116. 藤井孝藏, “動きだしたNASシステム,” 日本航空宇宙学会誌, Vol. 36, No. 414, pp. 323-325, 1988.
  • 117. 藤井孝藏, “航空機回りの遷音速流れの数値計算と可視化,” 日本可視化情報学会誌,Vol. 6, No. 21, pp. 122-127, 1986.
  • 118. 藤井孝藏, “大迎角剥離渦に関する数値計算,”日本航空宇宙学会誌, Vol. 33, No. 377号, pp. 339-350, 1985.
  • 119. 藤井孝藏, “NASA Ames Research Center における数値流体力学研究,” 日本航空宇宙学会誌, Vol. 33, No. 374, pp.147-149,1985.