All Stories

  1. Flow control strategy for stably generating vortex

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Takuto Ogawa, Aiko Yakeno

  2. Extraction of Speed-Control Strategy in En-Route Air Traffic using Multi-Objective Optimization and Decision Tree

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  3. Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder

    Article • AIP Advances, October 2021, American Institute of Physics

    Professor Kozo Fujii

  4. A high-fidelity body-force modeling approach for plasma-based flow control simulations

    Article • Physics of Fluids, March 2021, American Institute of Physics

    Professor Kozo Fujii

  5. Flow-Control Experiment around Half-Span Wing Model for DBD-PA Application on UAV

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  6. Flight Test of UAV with DBD-Pa Flow Control

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Hiroshi Yoneda, hiroki kato

  7. Mechanism of flow separation control with DBD plasma actuator obtained by Ape X Deep Q Network Control

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  8. Multi-Objective Takeoff Time Optimization Using Cellular Automaton-Based Simulator

    Article • IEEE Access, January 2021, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Kozo Fujii

  9. Computational Study of Wing-Tip Effect for Flow-Control Authority of Dielectric-Barrier-Discharge Plasma Actuator

    Article • AIAA Journal, November 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  10. Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil

    Article • AIAA Journal, October 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  11. Flow-control capability of electronic-substrate-sized power supply for a plasma actuator

    Article • Sensors and Actuators A Physical, May 2020, Elsevier

    Professor Kozo Fujii

  12. Separated Flow Control of Small Horizontal-Axis Wind Turbine Blades Using Dielectric Barrier Discharge Plasma Actuators

    Article • Energies, March 2020, MDPI AG

    Professor Kozo Fujii

  13. Flow Control on an Unmanned Aerial Vehicle Using a Plasma Actuator Driven By a Substrate-Size Power Supply

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  14. Aerodynamics of Owl-like Wing Model at Low Reynolds Numbers

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2020, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  15. Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6 × 106

    Article • Physics of Fluids, September 2019, American Institute of Physics

    Dr Hikaru Aono, Professor Kozo Fujii, Taku Nonomura, Makoto Sato, Aiko Yakeno

  16. Computational Study of Wing Tip Effect for the Flow Control Authority of DBD Plasma Actuator

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Prof. Makoto Yamamoto

  17. Preliminary Study of Multi-Objective Air Traffic Optimization by Using Step Back Cellular Automaton

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  18. Large eddy simulation of acoustic waves generated from a hot supersonic jet

    Article • Shock Waves, March 2019, Springer Science + Business Media

    Professor Kozo Fujii

  19. Aerodynamic drag reduction of a simplified vehicle model by promoting flow separation using plasma actuator

    Article • Mechanical Engineering Letters, January 2019, Japan Society of Mechanical Engineers

    Professor Kozo Fujii, Takuji Nakashima

  20. Dominant parameters for maximum velocity induced by body-force models for plasma actuators

    Article • Theoretical and Computational Fluid Dynamics, October 2018, Springer Science + Business Media

    Professor Kozo Fujii, Aiko Yakeno

  21. Three Flow Features behind the Flow Control Authority of DBD Plasma Actuator: Result of High-Fidelity Simulations and the Related Experiments

    Article • Applied Sciences, April 2018, MDPI AG

    Professor Kozo Fujii

  22. Identification of Acoustic Wave Propagation Pattern of a Supersonic Jet Using Frequency-Domain POD

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2018, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  23. Effect of Mach Number on Airfoil Characteristics at Reynolds Number of 3,000

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2018, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  24. Preliminary Study of Multi-Objective Air Traffic Optimization by using Step Back Cellular Automaton

    Article • The Proceedings of The Computational Mechanics Conference, January 2018, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  25. Aerodynamic drag reduction by controlling flow structure of simplified vehicle model using plasma actuator

    Article • The Proceedings of the Fluids engineering conference, January 2018, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  26. Plasma-Actuator Burst-Mode Frequency Effects on Leading-Edge Flow-Separation Control at Reynolds Number 2.6×105

    Article • AIAA Journal, November 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Dr Hikaru Aono, Taku Nonomura

  27. Characteristic finite-difference WENO scheme for multicomponent compressible fluid analysis: Overestimated quasi-conservative formulation maintaining equilibriums of velocity, pressure, and temperature

    Article • Journal of Computational Physics, July 2017, Elsevier

    Professor Kozo Fujii

  28. Study on the Sensing Parameters toward Better Feed-back Control of Stall Separation with DBD Plasma Actuator

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Takuto Ogawa

  29. Experimental Study on the Detailed Structure of Separation Bubble in Flow Control with DBD Plasma Actuator

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Taku Nonomura, Professor Kozo Fujii

  30. Burst-Mode Frequency Effects of Dielectric Barrier Discharge Plasma Actuator for Separation Control

    Article • AIAA Journal, April 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Taku Nonomura

  31. Large-Eddy Simulation of NACA 0015 Airfoil Flow at Reynolds Number of 1.6×106

    Article • AIAA Journal, February 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Taku Nonomura

  32. Spanwise modulation effects of local body force on downstream turbulence growth around two-dimensional hump

    Article • International Journal of Heat and Fluid Flow, February 2017, Elsevier

    Professor Kozo Fujii, Aiko Yakeno

  33. Experimental Study of Burst Ratio Effect for Dielectric-Barrier-Discharge Plasma Actuator for Separation Control

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  34. Control of dynamic flowfield around a pitching NACA633−618 airfoil by a DBD plasma actuator

    Article • International Journal of Heat and Fluid Flow, December 2016, Elsevier

    Professor Kozo Fujii

  35. Conservative high-order flux-reconstruction schemes on moving and deforming grids

    Article • Computers & Fluids, November 2016, Elsevier

    Professor Kozo Fujii

  36. Computational analysis of aeroacoustic noise generated from a rotating tire with a longitudinal groove

    Article • The Journal of the Acoustical Society of America, October 2016, Acoustical Society of America (ASA)

    Professor Kozo Fujii

  37. Analysis of nozzle geometry effect on supersonic jet noise using Schlieren

    Article • The Journal of the Acoustical Society of America, October 2016, Acoustical Society of America (ASA)

    Professor Kozo Fujii, AKIRA OYAMA

  38. Multi-Objective Aeroacoustic Design Exploration of Launch-Pad Flame Deflector Using Large-Eddy Simulation

    Article • Journal of Spacecraft and Rockets, July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Taku Nonomura

  39. Control of Dynamically Stalled Flowfield around a Pitching Airfoil by DBD Plasma Actuator

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Hikaru Aono, Professor Kozo Fujii, Dr Motofumi Tanaka

  40. Control of Airfoil Flow at Cruise Condition by DBD Plasma Actuator - Sophisticated Airfoil vs. Simple Airfoil with Flow Control -

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  41. Mach Number Dependence on Sound Sources in High Mach Number Turbulent Mixing Layer

    Article • May 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Taku Nonomura

  42. Effects of Disturbed Nozzle-exit Boundary Layers on Acoustic Waves from Ideally-expanded Supersonic Jet

    Article • May 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  43. Plate-Angle Effects on Acoustic Waves from Supersonic Jets Impinging on Inclined Plates

    Article • AIAA Journal, March 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Prof. Makoto Yamamoto, Prof. Shigeru Obayashi, Taku Nonomura

  44. Significance of Computational Spanwise Domain Length on LES for the Flowfield with Large Vortex Structure

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Hikaru Aono, Professor Kozo Fujii, Taku Nonomura

  45. Experimental Study of Effects of Frequency for Burst Wave on a DBD Plasma Actuator for Separation

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  46. High-speed jet noise

    Article • Mechanical Engineering Reviews, January 2016, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  47. Wall-Turbulence Structure with Pressure Gradient Around 2D Hump

    Article • January 2016, Springer Science + Business Media

    Professor Kozo Fujii, Aiko Yakeno

  48. Computational Analysis of Compressible Gas-Particle-Multiphase Turbulent Mixing Layer in Euler-Euler Formulation

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2016, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  49. Linear Stability Analyses and Large Eddy Simulations for Acoustic Wave Generation Mechanism of a Transitional Supersonic Jet

    Article • January 2016, Springer Science + Business Media

    Professor Kozo Fujii

  50. Two- and Three-Dimensional Numerical Analysis for Flow Field Characteristics at Various Low Reynolds Numbers

    Article • January 2016, Springer Science + Business Media

    Professor Kozo Fujii

  51. Computational Studies on Flow Separation Controls at Relatively Low Reynolds Number Regime

    Article • November 2015, World Scientific Pub Co Pte Lt

    Professor Kozo Fujii

  52. Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number

    Article • Physics of Fluids, November 2015, American Institute of Physics

    Professor Kozo Fujii, Aiko Yakeno

  53. Separation control based on turbulence transition around a two-dimensional hump at different Reynolds numbers

    Article • International Journal of Heat and Fluid Flow, October 2015, Elsevier

    Professor Kozo Fujii

  54. Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control

    Article • AIAA Journal, September 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Dr Hikaru Aono, Taku Nonomura, Aiko Yakeno

  55. Contribution of large-scale vortex and fine-scale turbulent structure in separated flow control using DBD plasma actuator

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  56. Nozzle-to-Ground Distance Effect on Nondominated Solutions of Multiobjective Aeroacoustic Flame Deflector Design Problem

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  57. Fully-conservative High-order FR Scheme on Moving and Deforming Grids

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  58. A Finite Difference WENO Scheme Maintaining Velocity, Pressure and Temperature Equilibrium in Multicomponent Compressible Fluid Analysis

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  59. A ranking method based on two preference criteria: Chebyshev function and ε-indicator

    Article • May 2015, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Kozo Fujii

  60. LES of transient flows controlled by DBD plasma actuator over a stalled airfoil

    Article • International Journal of Computational Fluid Dynamics, March 2015, Taylor & Francis

    Professor Kozo Fujii

  61. Mechanisms of surface pressure distribution within a laminar separation bubble at different Reynolds numbers

    Article • Physics of Fluids, February 2015, American Institute of Physics

    Professor Kozo Fujii

  62. Design Exploration of a DBD Plasma Actuator for Massive Separation Control

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Hikaru Aono, Professor Kozo Fujii

  63. LES of Separated-flow Controlled by DBD Plasma Actuator around NACA 0015 over Reynolds Number Range of 10^4-10^6

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Hikaru Aono, Professor Kozo Fujii, Aiko Yakeno

  64. Spatial Growth of the Spanwise Disturbance Induced by a Synthetic Jet on Separation Control over an Airfoil

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  65. Multiobjective Design Exploration of a Many-objective Space Trajectory Problem for Low-Thrust Spacecraft Using MOEA with Large Populations

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  66. Anion and cation dynamics of sulfonylamide-based ionic liquids and the solid–liquid transitions

    Article • Physical Chemistry Chemical Physics, January 2015, Royal Society of Chemistry

    Professor Kozo Fujii

  67. Comparison of Numerical Methods Evaluating Airfoil Aerodynamic Characteristics at Low Reynolds Number

    Article • Journal of Aircraft, January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Donghwi Lee, Taku Nonomura

  68. Generation of Acoustic Disturbances in Supersonic Laminar Cavity Flows

    Article • The International Journal of Acoustics and Vibration, January 2015, International Institute of Acoustics and Vibration (IIAV)

    Professor Kozo Fujii

  69. A new technique for freestream preservation of finite-difference WENO on curvilinear grid

    Article • Computers & Fluids, January 2015, Elsevier

    Professor Kozo Fujii

  70. Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air

    Article • Mechanical Engineering Journal, January 2015, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  71. On the freestream preservation of high-order conservative flux-reconstruction schemes

    Article • Journal of Computational Physics, January 2015, Elsevier

    Professor Kozo Fujii

  72. Relation Between Sound Sources and Vortical Structures in Isotropic Compressible Turbulence

    Article • November 2014, ASME International

    Professor Kozo Fujii

  73. Computational and Experimental Analysis of a High-Performance Airfoil Under Low-Reynolds-Number Flow Condition

    Article • Journal of Aircraft, November 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Dr Hikaru Aono, Taku Nonomura

  74. High-performance computing-based exploration of flow control with micro devices

    Article • Philosophical Transactions of the Royal Society A Mathematical Physical and Engineering Sciences, July 2014, Royal Society Publishing

    Professor Kozo Fujii

  75. Many-objective evolutionary computation for optimization of separated-flow control using a DBD plasma actuator

    Article • July 2014, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Kozo Fujii

  76. Effective Mechanisms for Turbulent-separation Control by DBD Plasma Actuator around NACA0015 at Reynolds Number 1,600,000

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Dr Hikaru Aono, Taku Nonomura

  77. LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Hikaru Aono, Professor Kozo Fujii, Taku Nonomura, Aiko Yakeno

  78. Geometric interpretations and spatial symmetry property of metrics in the conservative form for high-order finite-difference schemes on moving and deforming grids

    Article • Journal of Computational Physics, March 2014, Elsevier

    Professor Kozo Fujii

  79. A simple interface sharpening technique with a hyperbolic tangent function applied to compressible two-fluid modeling

    Article • Journal of Computational Physics, February 2014, Elsevier

    Professor Kozo Fujii

  80. Experimental Study of a Nano-second Pulse Plasma Actuator for Low Reynolds Number Flow Control

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  81. Effect of Burst Frequency and Reynolds Number on Flow Control Authority of DBD Plasma Actuator on NACA0012 Airfoil

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Dr Hikaru Aono

  82. Effects of Burst Frequency and Momentum Coefficient of DBD Actuator on Control of Deep-stall Flow around NACA0015 at Rec=2.6x10^{5}

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Dr Hikaru Aono

  83. Multiobjective Design Exploration of an Aeroacoustic Design Problem for Rocket Launch Site with Evolutionary Computation and Large Eddy Simulations

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, Prof. Makoto Yamamoto

  84. Computational Prediction of Acoustic Waves from a Subscale Rocket Motor

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2014, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  85. Computational Analysis of Aerodynamic Performance of Mars Airplane

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2014, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  86. Planetary Atmosphere Wind Tunnel Tests on Aerodynamic Characteristics of a Mars Airplane Scale Model

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2014, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  87. Control surface effectiveness of low Reynolds number flight vehicles

    Article • Journal of Fluid Science and Technology, January 2014, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  88. Analysis of Owl-like Airfoil Aerodynamics at Low Reynolds Number Flow

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2014, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  89. Institute of Theoretical and Applied Mechanics - Place for Human Resources for Innovation and Imagination

    Article • TRENDS IN THE SCIENCES, January 2014, Japan Science Support Foundation

    Professor Kozo Fujii

  90. Robust explicit formulation of weighted compact nonlinear scheme

    Article • Computers & Fluids, October 2013, Elsevier

    Professor Kozo Fujii

  91. Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings

    Article • AIAA Journal, September 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  92. Scaling Analysis of Propeller-Driven Aircraft for Mars Exploration

    Article • Journal of Aircraft, September 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  93. Mechanism of controlling supersonic cavity oscillations using upstream mass injection

    Article • Physics of Fluids, August 2013, American Institute of Physics

    Professor Kozo Fujii

  94. DBD Plasma Actuator Multi-Objective Design Optimization at Reynolds Number 63,000: Baseline Case

    Article • July 2013

    Professor Kozo Fujii

  95. Plasma Flow Control Simulation of an Airfoil of Wind Turbine at an Intermediate Reynolds Number

    Article • July 2013

    Professor Kozo Fujii, Aiko Yakeno

  96. Large-Eddy Simulations of Owl-Like Wing Under Low Reynolds Number Conditions

    Article • July 2013

    Professor Kozo Fujii

  97. A New Technique for Finite Difference WENO with Geometric Conservation Law

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  98. Effect of Wing Planform on Aerodynamic Characteristics at Low Reynolds Numbers using a Low Density Wind Tunnel

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  99. Significance of Three-dimensional Unsteady Flows inside the Cavity on Separated-flow Control around an NACA0015 using a Synthetic Jet

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  100. Massive Parametric Study by LES on Separated-flow Control around Airfoil using DBD Plasma Actuator at Reynolds Number 63,000

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  101. Space trajectory design: Analysis of a real-world many-objective optimization problem

    Article • June 2013, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Kozo Fujii

  102. Effects of Inflow Shear Layer Parameters on a Transitional Supersonic Jet with a Moderate Reynolds Number

    Article • May 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  103. On the feedback mechanism in supersonic cavity flows

    Article • Physics of Fluids, May 2013, American Institute of Physics

    Professor Kozo Fujii

  104. Control Mechanism of Plasma Actuator for Separated Flow around NACA0015 at Reynolds Number 63,000 -Separation Bubble Related Mechanisms-

    Article • January 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  105. A non-equilibrium dynamic wall-model for LES of high Reynolds number airfoil flow near stall condition

    Article • January 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  106. Feedback Mechanism in Supersonic Laminar Cavity Flows

    Article • AIAA Journal, January 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  107. A New Multiobjective Genetic Programming for Extraction of Design Information from Non-dominated Solutions

    Article • January 2013, Springer Science + Business Media

    Professor Kozo Fujii

  108. An Alternative Preference Relation to Deal with Many-Objective Optimization Problems

    Article • January 2013, Springer Science + Business Media

    Professor Kozo Fujii

  109. Conservative metric evaluation for high-order finite difference schemes with the GCL identities on moving and deforming grids

    Article • Journal of Computational Physics, January 2013, Elsevier

    Professor Kozo Fujii

  110. Large-Eddy Simulation of Low-Reynolds-Number Flow Over Thick and Thin NACA Airfoils

    Article • Journal of Aircraft, January 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  111. Analysis of Acoustic-Fields Generated by a Supersonic Jet Impinging on Flat and Curved Inclined Plates

    Article • International Journal of Aerospace and Lightweight Structures (IJALS) -, January 2013, Research Publishing Services

    Professor Kozo Fujii

  112. Burst Frequency Effect of DBD Plasma Actuator on the Control of Separated Flow over an Airfoil

    Article • June 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  113. Computational Analysis of Vortex Structures Induced by a Synthetic Jet to Control Separated Flows

    Article • International Journal of Flow Control, June 2012, Multi-Science Publishing Co. Ltd.

    Professor Kozo Fujii

  114. Numerical (error) issues on compressible multicomponent flows using a high-order differencing scheme: Weighted compact nonlinear scheme

    Article • Journal of Computational Physics, April 2012, Elsevier

    Professor Kozo Fujii

  115. Comparative Study of Co-flow and Counter Blowing DBD Plasma Actuators for Separated Flow over an Airfoil

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  116. Noise Control of Supersonic Cavity Flow with Upstream Mass Blowing

    Article • January 2012, Springer Science + Business Media

    Professor Kozo Fujii

  117. Role of RANS, Hybrid and LES for Wing Flow Simulations at Relatively Low Reynolds Numbers

    Article • January 2012, Springer Science + Business Media

    Professor Kozo Fujii

  118. Computational Study of Effects of Nondimensional Parameters on Synthetic Jets

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2012, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  119. Aerodynamic Design Exploration for Reusable Launch Vehicle Using Genetic Algorithm with Navier Stokes Solver

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2012, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  120. An Effective Three-Dimensional Layout of Actuation Body Force for Separation Control

    Article • International Journal of Aerospace Engineering, January 2012, Hindawi Publishing Corporation

    Professor Kozo Fujii

  121. Numerical Investigation of Asymmetric Separation Vortices over Slender Body by RANS/LES Hybrid Simulation

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN, January 2012, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  122. Overexpansion Effects on Characteristics of Mach Waves from a Supersonic Cold Jet

    Article • AIAA Journal, October 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  123. Mechanism of acoustic radiation from Supersonic Jets Impinging to Inclined Flat Plates

    Article • The Journal of the Acoustical Society of America, October 2011, Acoustical Society of America (ASA)

    Professor Kozo Fujii

  124. Validation study on computational aeroacoustics of acoustic waves from sub-scale rocket plumes

    Article • The Journal of the Acoustical Society of America, October 2011, Acoustical Society of America (ASA)

    Professor Kozo Fujii

  125. Aeroacoustic Waves Generated from a Supersonic Jet Impinging on an Inclined Flat Plate

    Article • International Journal of Aeroacoustics, August 2011, SAGE Publications

    Professor Kozo Fujii

  126. Effects of Plate Angles on Acoustic Waves from a Supersonic Jet Impinging on an Inclined Flat Plate

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  127. Experimental Study of Effects of Frequency for Burst Wave on DBD Plasma Actuator for Separation Control

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  128. Computational Study of Effects of Near-wall Turbulent Structure on Aeroacoustic Waves from a Supersonic Jet Impinging on a Inclined Plate

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  129. Multidisciplinary and Multi-objective Design Exploration Methodology for Conceptual Design of a Hybrid Rocket

    Article • March 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  130. Multiobjective Design Exploration in Space Engineering

    Article • January 2011, IntechOpen

    Professor Kozo Fujii, AKIRA OYAMA

  131. Effects of Shear-Layer Characteristic on the Feedback-loop Mechanism in Supersonic Open Cavity Flows

    Article • January 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  132. Effective Three-dimensional Layout of Imaginary Body Force for Separation Control

    Article • January 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  133. Mach Number Effects on Vortex Breakdown in Subsonic Flow over a Delta Wing

    Article • January 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  134. Features of Frontier Research: Consideration from the Characteristics of Space Engineering

    Article • TRENDS IN THE SCIENCES, January 2011, Japan Science Support Foundation

    Professor Kozo Fujii

  135. Computational Study of Aerodynamic Characteristics of an Airfoil With DBD Plasma Actuator

    Article • January 2011, ASME International

    Professor Kozo Fujii

  136. Three-Dimensional Wing Design Towards the Future Mars Airplane

    Article • January 2011, ASME International

    Professor Kozo Fujii

  137. Aerodynamic Design Exploration for Reusable Launch Vehicle Using Multi-Objective Genetic Programming

    Article • January 2011, ASME International

    Professor Kozo Fujii

  138. Large-Eddy Simulation of the Flow over a Thin Airfoil at Low Reynolds Number

    Article • January 2011, Springer Science + Business Media

    Professor Kozo Fujii

  139. Aerodynamic Multiobjective Design Exploration of Flapping Wing Using a Navier–Stokes Solver

    Article • January 2011, Springer Science + Business Media

    Professor Kozo Fujii

  140. Experimental Study of Blowing Direction Effects of DBD Plasma Actuator on Separation Control of Flow Around an Airfoil

    Article • January 2011, ASME International

    Professor Kozo Fujii

  141. Computational Study of Flow Characteristics of Thick and Thin Airfoil With Implicit Large-Eddy Simulation at Low Reynolds Number

    Article • January 2011, ASME International

    Professor Kozo Fujii

  142. An Acoustic Impedance Model for Evaluating the Ground Effect of Static-Firing Tests on a Rocket Motor

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2011, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  143. Toward accurate simulation and analysis of strong acoustic wave phenomena-A review from the experience of our study on rocket problems

    Article • International Journal for Numerical Methods in Fluids, October 2010, Wiley

    Professor Kozo Fujii

  144. Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition

    Article • Journal of Aircraft, September 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  145. Recent Efforts in Rocket Plume Acoustics

    Article • July 2010, World Scientific Pub Co Pte Lt

    Professor Kozo Fujii

  146. Computational Analysis of Unsteady Flow-Field Induced by Plasma Actuator in Burst Mode

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  147. Aerodynamic Shape Design of the Vertical Landing Rocket Vehicle

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  148. LES Study of Feedback-loop Mechanism of Supersonic Open Cavity Flows

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  149. POD of Aeroacoustic Fields of a Jet Impinging on an Inclined Plate

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  150. Computational Analysis of Mach Number Effects on the Edgetone Phenomenon

    Article • AIAA Journal, June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  151. Freestream and vortex preservation properties of high-order WENO and WCNS on curvilinear grids

    Article • Computers & Fluids, February 2010, Elsevier

    Professor Kozo Fujii

  152. Acoustic Waves from a Supersonic Jet Impinging on an Inclined Flat Plate

    Article • January 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  153. Flow Field Data Mining of Pareto-Optimal Airfoils Using Proper Orthogonal Decomposition

    Article • January 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  154. Computational Study of the Synthetic Jet on Separated Flow Over a Backward-Facing Step

    Article • January 2010, ASME International

    Professor Kozo Fujii

  155. Computational Study on Effect of Synthetic Jet Design Parameters

    Article • International Journal of Aerospace Engineering, January 2010, Hindawi Publishing Corporation

    Professor Kozo Fujii

  156. An Acoustic Impedance Model for Evaluating Ground Effect of Static-Firing Tests on Rocket Motors

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2010, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  157. Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition

    Article • June 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  158. Effects of difference scheme type in high-order weighted compact nonlinear schemes

    Article • Journal of Computational Physics, June 2009, Elsevier

    Professor Kozo Fujii

  159. Aerodynamic Multiobjective Design Exploration of a Flapping Airfoil Using a Navier-Stokes Solver

    Article • Journal of Aerospace Information Systems, March 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  160. Computational Analysis of Characteristics of Mach Wave Sources in Supersonic Free-Jets

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  161. Detailed Analysis of Flat Plate Pressure Peaks Created by Supersonic Jet Impingements

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  162. Improvements in the Reliability and Efficiency of Body-fitted Cartesian Grid Method

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  163. Airfoil Flow Experiment on the Duty Cycle of DBD Plasma Actuator

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  164. Uniform Flow Preserving Property of High Order Upwind Finite Difference Schemes on Generalized Coordinate System

    Article • January 2009, Springer Science + Business Media

    Professor Kozo Fujii

  165. Propulsion by an Oscillating Thin Airfoil at Low Reynolds Number

    Article • January 2009, Springer Science + Business Media

    Professor Kozo Fujii

  166. Computational Study of Frequency and Amplitude Effects on Separation Flow Control With the Synthetic Jet

    Article • January 2009, ASME International

    Professor Kozo Fujii

  167. Numerical Analysis for Magnetic Control of Heat-Transfer and Pressure in Hypersonic Shock Wave Interference Flows

    Article • January 2009, Springer Science + Business Media

    Professor Kozo Fujii

  168. Data mining of non-dominated solutions using proper orthogonal decomposition

    Article • January 2009, ACM (Association for Computing Machinery)

    Professor Kozo Fujii

  169. Flashback: 30 Years Numerical Fluid Mechanics and Aerodynamics in Japan, other Asian Countries and the Western Pacific Rim

    Article • January 2009, Springer Science + Business Media

    Professor Kozo Fujii

  170. Mach Number and Temperature Effects on Mach Wave Emission from Supersonic Jets

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  171. Development of Multi-Objective Six Sigma Approach for Robust Design Optimization

    Article • Journal of Aerospace Information Systems, August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  172. CFD contributions to high-speed shock-related problems

    Article • Shock Waves, June 2008, Springer Science + Business Media

    Professor Kozo Fujii

  173. Over-expansion Effects on Mach 3.0 Supersonic Jet Acoustics

    Article • May 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  174. Aerodynamic Characteristics of a Delta Wing at High Angles of Attack

    Article • April 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii, AKIRA OYAMA

  175. Compact Scheme with Filtering for Large-Eddy Simulation of Transitional Boundary Layer

    Article • AIAA Journal, March 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  176. Mach Number Effect on Flowfield Over a Delta Wing in Supersonic Region

    Article • January 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  177. Generation and Propagation of Pressure Waves from H-IIA Launch Vehicle at Lift-Off

    Article • January 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  178. Computational Analysis of Noise Sources Inside Turbulent Boundary Layer Over a Generalized Bump

    Article • January 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  179. Visualization and Verification Method for Failure Network Analysis of Space Launch Vehicles

    Article • January 2008, ASME International

    Professor Kozo Fujii

  180. Computational Analysis of Supersonic Underexpanded Jets Impinging on an Inclined Flat Plate

    Article • June 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  181. Compact Differencing and Filtering Schemes for Large-Eddy Simulation of Compressible Transitional Boundary Layer

    Article • June 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  182. A Study on Flapping Motion for MAV Design Using Design Exploration

    Article • May 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  183. Multi-Objective Six Sigma Approach Applied to Robust Airfoil Design for Mars Airplane

    Article • April 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  184. Increasing Order of Accuracy of Weighted Compact Non-Linear Scheme

    Article • January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  185. Effective Layout of Plasma Actuators for a Flow Separation Control on a Wing

    Article • January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  186. Study on the Automated CFD Analysis Tools for Conceptual Design of Space Transportation Vehicles

    Article • January 2007, ASME International

    Professor Kozo Fujii

  187. Computational Analysis of Noise Sources Inside the High Speed Flow Over a Bump

    Article • January 2007, ASME International

    Professor Kozo Fujii

  188. Influence of Stores on the Transonic Flutter of a Delta Wing Configuration

    Article • AIAA Journal, January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  189. Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows

    Article • AIAA Journal, January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  190. Computational Analysis of Characteristics and Mach Number Effects on Noise Emission From Ideally Expanded Highly Supersonic Free-Jet

    Article • January 2007, ASME International

    Professor Kozo Fujii

  191. Computational Aeroacoustic Analysis of Overexpanded Supersonic Jet Impingement on a Flat Plate With/Without Hole

    Article • January 2007, ASME International

    Professor Kozo Fujii

  192. New Constraint-Handling Method for Multi-Objective and Multi-Constraint Evolutionary Optimization

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2007, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  193. Effects of Plasma Actuator Layouts on a Flow Separation Control over a Wing

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 2007, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  194. Large-Eddy Simulation of Compressible Transitional Boundary Layer

    Article • November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  195. Experimental Study of Underexpanded Supersonic Jet Impingement on an Inclined Flat Plate

    Article • AIAA Journal, November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  196. Computational Analysis of Mach Number Effects on Edgetone

    Article • June 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  197. A Study on Airfoil Design for Future Mars Airplane

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  198. Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  199. Flow Field Analysis of Jet Impinging on an Inclined Flat Plate at High Plate Angles

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  200. Computational Aerodynamic Analysis of Capsule Configurations Toward the Development of Reusable Rockets

    Article • Journal of Spacecraft and Rockets, January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  201. Announcements, Comments, and Acknowledgments

    Article • AIAA Journal, January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  202. Improvement of noise filtering and image registration methods for the Pressure Sensitive Paint experiments

    Article • Journal of Visualization, September 2005, Springer Science + Business Media

    Professor Kozo Fujii

  203. Progress and future prospects of CFD in aerospace—Wind tunnel and beyond

    Article • Progress in Aerospace Sciences, August 2005, Elsevier

    Professor Kozo Fujii

  204. Pareto-Optimality-Based Constraint-Handling Technique and Its Application to Compressor Design

    Article • June 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  205. Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows

    Article • June 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  206. Computational Study of a Supersonic Base Flow Using Hybrid Turbulence Methodology

    Article • AIAA Journal, June 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  207. Analysis and Prediction of Thin-Airfoil Stall Phenomena with Hybrid Turbulence Methodology

    Article • AIAA Journal, May 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  208. PSP Measurements in the Large-Scale Transonic Wind Tunnel and Associated Image Data Processing

    Article • January 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  209. Numerical Analysis of the Aerodynamic Characteristics of SSTO Configurations with an Aerospike Nozzle

    Article • January 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  210. Computational Analysis of Various Factors on the Edgetone Mechanism Using High Order Schemes

    Article • January 2005, ASME International

    Professor Kozo Fujii

  211. New Developments in Computational Fluid Dynamics

    Article • January 2005

    Professor Kozo Fujii

  212. Assessment of CFD Estimation of Aerodynamic Characteristics of Basic Reusable Rocket Configurations

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2005, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  213. Flow Field Analysis of Under-Expanded Supersonic Jets Impinging on an Inclined Flat Plate: Analysis With PSP/Schlieren Images and CFD Simulations

    Article • January 2005, ASME International

    Professor Kozo Fujii

  214. Visualization for CFD Research-Past and Future

    Article • Journal of the Visualization Society of Japan, January 2005, The Visualization Society of Japan

    Professor Kozo Fujii

  215. Library-less Realtime Visualization System and its Use

    Article • Journal of the Visualization Society of Japan, January 2005, The Visualization Society of Japan

    Professor Kozo Fujii

  216. Development of Postprocessing Software for PSP/TSP Pressure Measurement System

    Article • Journal of the Visualization Society of Japan, January 2005, The Visualization Society of Japan

    Professor Kozo Fujii

  217. B303 感圧・感温塗料を用いた斜め平板衝突噴流の解析

    Article • Journal of the Visualization Society of Japan, January 2005, The Visualization Society of Japan

    Professor Kozo Fujii

  218. Effect of the Time Stepping Size in the Implicit Method for Transonic Flutter Simulations

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 2005, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  219. Development of Realistic Optimization Method of TSTO Spaceplane - Multi-Objective and Robust Optimization

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  220. Numerical Investigations of the Side Fence Effect on Linear Plug Nozzle Performance

    Article • July 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  221. High-Order Compact Difference Scheme Applied to Double-Delta Wing Vortical Flows

    Article • Journal of Aircraft, July 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  222. Effects of Number of Stores on the Transonic Flutter Characteristics of a Delta Wing Configuration

    Article • June 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  223. Prediction of a Thin-Airfoil Stall Phenomenon Using LES/RANS Hybrid Methodology with Compact Difference Scheme

    Article • June 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  224. Computational Study of a Supersonic Base Flow Using LES/RANS Hybrid Methodology

    Article • January 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  225. Flow Field and Performance Analysis of Aerospike Nozzles with Simplified Clustered Modules

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2004, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  226. PSP measurements of the pressure fields over the a complicated model configuration

    Article • Journal of the Visualization Society of Japan, January 2004, The Visualization Society of Japan

    Professor Kozo Fujii

  227. Computational Analysis of the Effective Secondary-Flow Injections for the Plug-Nozzle Drag Reduction

    Article • June 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  228. Application of High-Order Compact Difference Scheme to Vortical Flow Computation over a Delta and Double-Delta Wings

    Article • June 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  229. Flow Classification of the Under-Expanded Super Sonic Jet Impinging on a Flat Plate

    Article • June 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  230. CFD Prediction of the Aerodynamic Characteristics of Capsule-Like Configurations for the Future SSTO Development

    Article • January 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  231. Compressible Flow Simulations Over Basic Reusable Rocket Configurations

    Article • January 2003, ASME International

    Professor Kozo Fujii

  232. Improvement of the Noise Filtering and Image Registration Methods for PSP Experiments

    Article • January 2003, ASME International

    Professor Kozo Fujii

  233. Numerical Estimations of Transonic Flutter Calculation with the Fluid/Structure Coupling Method

    Article • January 2003, Springer Science + Business Media

    Professor Kozo Fujii

  234. Numerical Analysis of the Clustered Type Aerospike Nozzle Flow: Flow Structures and Thrust Performance

    Article • January 2003, Springer Science + Business Media

    Professor Kozo Fujii

  235. Flow Field and Performance Analysis of an Annular-Type Aerospike Nozzle with Base Bleeding.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2003, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  236. Establishment of the PSP measurement system using Ruthenium(II) complex

    Article • Journal of the Visualization Society of Japan, January 2003, The Visualization Society of Japan

    Professor Kozo Fujii

  237. On Post Image Processing for Pressure Sensitive Paint

    Article • Journal of the Visualization Society of Japan, January 2003, The Visualization Society of Japan

    Professor Kozo Fujii

  238. Mechanism of Dynamic Instability of a Reentry Capsule at Transonic Speeds

    Article • AIAA Journal, December 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  239. Visualization of Jet Flows over a Plate by Pressure-Sensitive Paint Experiments and Comparison with CFD

    Article • Annals of the New York Academy of Sciences, October 2002, Wiley

    Professor Kozo Fujii

  240. The Effect of Module Clustering on Aerospike Nozzle Performance

    Article • June 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  241. Computational Analysis of the Secondary Flow Injection for the Drag Reduction of the Plug Nozzle

    Article • June 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  242. Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structures and Thrust Performance

    Article • Journal of Propulsion and Power, March 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  243. Numerical Investigations of the Base-Flow Characteristics of Axisymmetric Aerospike Nozzles.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2002, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  244. Computational Analysis of the Flow Field Near the Boat-tail Region of Annular Plug Nozzles.

    Article • JSME International Journal Series B, January 2002, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  245. On Post Image Processing for Pressure Sensitive Paint

    Article • Journal of the Visualization Society of Japan, January 2002, The Visualization Society of Japan

    Professor Kozo Fujii

  246. Assessment of the Reliability of CFD simulations for Delta wings Using Visualization Post Processings

    Article • Journal of the Visualization Society of Japan, January 2002, The Visualization Society of Japan

    Professor Kozo Fujii

  247. Computation of the Flow Field around Arbitrary Three-Dimensional Body Geometry Using Cartesian Grid.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 2002, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  248. CFD Applications to Space Transportation Sytems

    Article • December 2001, World Scientific Pub Co Pte Lt

    Professor Kozo Fujii

  249. Lessons Learned from the Blast Wave Computation Using Overset Moving Grids: Grid Motion Improves the Resolution

    Article • December 2001, World Scientific Pub Co Pte Lt

    Professor Kozo Fujii

  250. Flow field and performance analysis of the simplified clustered aerospike nozzles

    Article • June 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  251. Computers and flow visualization

    Article • Journal of Visualization, June 2001, Springer Science + Business Media

    Professor Kozo Fujii

  252. Computational analysis of the flow field near the boat-tail region of annular plug nozzles

    Article • April 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  253. Numerical Analysis of Dynamic Stability of a Reentry Capsule at Transonic Speeds

    Article • AIAA Journal, April 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  254. Flow field analysis of the base region of axisymmetric aerospike nozzles

    Article • January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  255. Real-Time Computation and Visualization on Mobile PC’s

    Article • January 2001, Springer Science + Business Media

    Professor Kozo Fujii

  256. A Visualization Technique to Identify the Flow Mechanism of Complicated Unsteady Flows

    Article • January 2001, Springer Science + Business Media

    Professor Kozo Fujii

  257. Numerical analysis of dynamic stability of a reentry capsule at transonic speeds

    Article • AIAA Journal, January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  258. PSP Measurement of the Jet Impingement Flow Field over a Flat Plate

    Article • Journal of the Visualization Society of Japan, January 2001, The Visualization Society of Japan

    Professor Kozo Fujii

  259. Study on the mechanism of the instability of a re-entry capsule at transonic speeds

    Article • June 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  260. Computational study of the flow field behind blunt capsules at transonic speeds

    Article • June 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  261. Computations of the axisymmetric plug nozzle flow fields - Flow structures and thrust performance

    Article • June 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  262. Numerical analysis of three-dimensional shock/shock interactions and the aerodynamic heating

    Article • January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  263. Recent Development of Aerodynamic Design Methodologies

    Article • January 1999

    Professor Kozo Fujii

  264. Efficiency improvement of unified implicit relaxation/time integration algorithms

    Article • AIAA Journal, January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  265. Efficiency Improvement of Unified Implicit Relaxation/Time Integration Algorithms

    Article • AIAA Journal, January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  266. 論文「Ｒｏｅの近似Ｒｉｅｍａｎｎ ｓｏｌｖｅｒの収束性に関する一考察」に対する質問

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 1999, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  267. COMPUTATIONS OF BLAST WAVE PROPAGATION USING AN OVERSET MOVING ZONAL METHOD

    Article • November 1998, World Scientific Pub Co Pte Lt

    Professor Kozo Fujii

  268. What Have We Learned from Computational Fluid Dynamics Research on Train Aerodynamics?

    Article • November 1998, World Scientific Pub Co Pte Lt

    Professor Kozo Fujii

  269. Prediction Method of Unsteady Combustion Around Hypersonic Projectile in Stoichiometric Hydrogen-Air

    Article • AIAA Journal, October 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  270. Three-Dimensional Flow Computation Around a Projectile Overtaking a Preceding Shock Wave

    Article • Journal of Spacecraft and Rockets, September 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  271. Numerical analysis of dynamic stability of a reentry capsule at transonic speeds

    Article • August 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  272. Prediction method of unsteady combustion around hypersonic projectile in stoichiometric hydrogen-air

    Article • AIAA Journal, January 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  273. Numerical investigation of three-dimensional compressible flows induced by a train moving into a tunnel

    Article • Computers & Fluids, July 1997, Elsevier

    Professor Kozo Fujii

  274. Numerical investigation of the one-dimensional piston supported detonation waves

    Article • Energy Conversion and Management, July 1997, Elsevier

    Professor Kozo Fujii

  275. Efficiency improvements of unified implicit relaxation/time integration algorithms and their applications

    Article • June 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  276. Three-dimensional computation of the flow induced by a projectile overtaking a shock wave

    Article • June 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  277. Cavity Flow with a Shock Wave Interaction in a Supersonic Duct.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1997, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  278. Numerical Analysis of a Three-Dimensional Cavity Flow Field in a Supersonic Duct.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1997, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  279. Detailed mechanism of the unsteady combustion around hypersonic projectiles

    Article • AIAA Journal, October 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  280. Enhancement of the leading-edge separation vortices by trailing-edge lateral blowing

    Article • AIAA Journal, September 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  281. First Damkoehler parameter for prediction and classification of unsteady combustions around hypersonic projectiles

    Article • July 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  282. Unsteady behavior of the shock wave passing over two and three dimensional obstacles

    Article • June 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  283. Flow Visualization in Computational Fluid Dynamics.

    Article • The Journal of the Japan Society of Aeronautical Engineering, January 1996, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  284. Flow Characteristics around the Cavity in a Supersonic Duct.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1996, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  285. Theoretical Algorithm to Design a Train Shape for Alleviating the Booming Noise at a Tunnel Exit.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1996, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  286. Aerodynamics of high speed trains passing by each other

    Article • Computers & Fluids, November 1995, Elsevier

    Professor Kozo Fujii

  287. Computational study of large-disturbance oscillations in unsteady supersonic combustion around projectiles

    Article • AIAA Journal, October 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  288. Examination of the improved model for the unsteady combustion around hypersonic projectiles

    Article • July 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  289. Experimental investigation of supersonic internal cavity flows

    Article • June 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  290. Three-dimensional adaptive bisection of unstructured grids for transient compressible flow computations

    Article • June 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  291. Numerical simulation of the flow around a projectile passing through a shock wave

    Article • June 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  292. Flow features of shock-induced combustion around projectile traveling at hypervelocities

    Article • AIAA Journal, June 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  293. Unified Zonal Method Based on the Fortified Solution Algorithm

    Article • Journal of Computational Physics, April 1995, Elsevier

    Professor Kozo Fujii

  294. Numerical investigation of supersonic flows around a spiked blunt body

    Article • Journal of Spacecraft and Rockets, January 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  295. Prediction of Wavefront of Compression Wave Generated by a Train Moving into a Tunnel with Steady Flow.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1995, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  296. On-dimensional Numerical Simulation of a Compression Wave Induced by a Train Entering a Tunnel.

    Article • TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, January 1995, Japan Society of Mechanical Engineers

    Professor Kozo Fujii

  297. Enhancement of the leading-edge separation vortices by the trailing-edge lateral blowing

    Article • January 1994, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  298. Computational study of unsteady combustion around projectiles with emphasis on the large-disturbance oscillation

    Article • January 1994, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  299. SIMULATION OF EXPERIMENTAL VISUALIZATION METHODS FOR COMPUTATIONAL FLUID DYNAMICS RESEARCH

    Article • International Journal of Computational Fluid Dynamics, January 1994, Taylor & Francis

    Professor Kozo Fujii

  300. Conservation law for moving and transformed grids

    Article • July 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  301. Numerical experiment of the flight trajectory simulation by fluid dynamics and flight dynamics coupling

    Article • July 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  302. Numerical Simulation of Compressible Flow Induced by a Train Moving in a Tunnel

    Article • July 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  303. Nonequilibrium turbulence modeling study on light dynamic stall of aNACA0012 airfoil

    Article • Journal of Aircraft, May 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  304. Flow features of shock-induced combustion around projectile travelling at hypervelocities

    Article • January 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  305. Numerical investigation of supersonic flows around a spiked blunt-body

    Article • January 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  306. Supercomputers and Their Performance in Computational Fluid Dynamics

    Article • January 1993, Springer Science + Business Media

    Professor Kozo Fujii

  307. Navier-Stokes Benchmark Tests

    Article • January 1993, Springer Science + Business Media

    Professor Kozo Fujii

  308. Visualization Technique in Computational Fluid Dynamics for Rational Comparison with Experiment

    Article • January 1992, Springer Science + Business Media

    Professor Kozo Fujii

  309. Recent Applications of the FNS Zonal Method to Complex Flow Problems

    Article • September 1991, SAE International

    Professor Kozo Fujii

  310. Numerical Simulations of Hypersonic Real-Gas Flows Over Space Vehicles

    Article • September 1991, SAE International

    Professor Kozo Fujii

  311. Unified zonal method based on the fortified Navier-Stokes concept

    Article • June 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  312. Supersonic inlet flow computations using fortified Navier-Stokes approach

    Article • June 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  313. Navier-Stokes simulation of two and three dimensional jets in crossflow

    Article • June 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  314. Numerical Simulation and Visualization for High Speed Flows

    Article • Journal of the Visualization Society of Japan, January 1991, The Visualization Society of Japan

    Professor Kozo Fujii

  315. Visualization for computational fluid dynamics and the comparison with experiments

    Article • August 1990, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  316. Newly constructed high speed wind tunnel at the Institute of Space and Astronautical Science (ISAS) and related activities

    Article • August 1990, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  317. Supercomputers and Workstations in Fluid Dynamic Research

    Article • January 1990, Springer Science + Business Media

    Professor Kozo Fujii

  318. High-resolution upwind scheme for vortical-flow simulations

    Article • Journal of Aircraft, December 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  319. Numerical simulation of vortical flows over a strake-delta wing

    Article • AIAA Journal, September 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  320. Navier-Stokes computations of the supersonic flows about a Space-Plane

    Article • August 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  321. Use of high-resolution upwind scheme for vortical flow simulations

    Article • June 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  322. Numerical study of the effect of tangential leading edge blowing on delta wing vortical flow

    Article • January 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  323. Computational fluid dynamics: Recent topics and the trend.

    Article • The Journal of the Japan Society of Aeronautical Engineering, January 1989, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  324. A method to increase the accuracy of vortical flow simulations

    Article • June 1988, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  325. Navier Stokes computation of the flow field over delta wings with spanwise leading edge blowing

    Article • June 1988, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  326. Numerical Aerodynamic Simulation Facility Takes Off

    Article • The Journal of the Japan Society of Aeronautical Engineering, January 1988, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  327. Navier-Stokes simulations of transonic flows over a wing-fuselage combination

    Article • AIAA Journal, December 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  328. Numerical simulation of vortical flows over a strake-delta wing

    Article • June 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  329. Toward the Navier-Stokes analysis of transport aircraft configurations

    Article • March 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  330. Navier-Stokes computations of transonic flows using the LU-A

    Article • March 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  331. Navier-Stokes simulations of transonic flows over a practical wing configuration

    Article • AIAA Journal, March 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Kozo Fujii

  332. Viscous Compressible Flow Simulations Using Supercomputers

    Article • January 1986, Springer Science + Business Media

    Professor Kozo Fujii

  333. Computation of viscous transonic flows about aircrafts and its visulization.

    Article • JOURNAL OF THE FLOW VISUALIZATION SOCIETY OF JAPAN, January 1986, The Visualization Society of Japan

    Professor Kozo Fujii

  334. Recent computational fluid dynamics works about high angle of attack aerodynamics with separations vortex.

    Article • The Journal of the Japan Society of Aeronautical Engineering, January 1985, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  335. Computational Fluid Dynamics Study at NASA Ames Research Center

    Article • The Journal of the Japan Society of Aeronautical Engineering, January 1985, Japan Society for Aeronautical and Space Sciences

    Professor Kozo Fujii

  336. Accurate simulation of vortical flows

    Article • Springer Science + Business Media

    Professor Kozo Fujii

  337. Improvement of the Optimization Method of the TSTO Configuration — Application of Accurate Aerodynamics

    Article • Springer Science + Business Media

    Professor Kozo Fujii

  338. Numerical Approach to the Analysis of Internal Pressure of M–V Rocket Fairing

    Article • Springer Science + Business Media

    Professor Kozo Fujii

  339. Simultaneous solutions of inviscid flow and boundary layer at transonic speeds

    Article • Springer Science + Business Media

    Professor Kozo Fujii

  340. An efficient four-factored time integration scheme for three-dimensional compressible flow problems

    Article • Springer Science + Business Media

    Professor Kozo Fujii

  341. Simulations of unsteady shock wave reflections using adaptive unstructured grids

    Article • Springer Science + Business Media

    Professor Kozo Fujii

  342. Visualization method for computational fluid dynamics with emphasis on the comparison with experiments

    Article • Springer Science + Business Media

    Professor Kozo Fujii