All Stories

  1. Hybrid Rocket Engine Design Using Pairwise Ranking Surrogate-assisted Differential Evolution

    Article • July 2023, ACM (Association for Computing Machinery)

    Dr Masahiro Kanazaki

  2. Improved Solution Search Performance of Constrained MOEA/D Hybridizing Directional Mating and Local Mating

    Article • April 2023, ACM (Association for Computing Machinery)

    Dr Masahiro Kanazaki

  3. Feedback-Circulating Design Space Exploration by Multi-Sampling Kriging Model

    Article • April 2023, ACM (Association for Computing Machinery)

    Kazuhisa Chiba, Dr Masahiro Kanazaki

  4. Numerical Analysis on Hovering Performance of Hexacopter “HAMILTON” for Mars Exploration

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

    Dr Masahiro Kanazaki, Makoto Sato

  5. Numerical investigation of wake structures of an atmospheric entry capsule by modal analysis

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

    Dr Masahiro Kanazaki

  6. Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport

    Article • March 2019, ACM (Association for Computing Machinery)

    Dr Masahiro Kanazaki

  7. Modal Decomposition Analysis of Subsonic Unsteady Flow Around An Atmospheric Entry Capsule with Forced Oscillation

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

    Dr Masahiro Kanazaki

  8. Evolutionary Multidisciplinary Design Optimization of Blended-Wing-Body-Type Flyback Booster

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

    Dr Masahiro Kanazaki

  9. Plume Effect of Flowfield Around Winged Two-Stage-To-Orbit and Its Flight Characteristics

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

    Dr Masahiro Kanazaki

  10. Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design

    Article • Engineering Optimization, September 2017, Taylor & Francis

    Dr Masahiro Kanazaki

  11. Planform Dependency of Optimum Supersonic Airfoil for Wing-Body-Nacelle Configuration Using Multi-Fidelity Design Optimization

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

    Dr Masahiro Kanazaki, Yoshikazu Makino

  12. Numerical Study of Coherent Structures Around a Re-entry Capsule using Proper Orthogonal Decomposition

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

    Dr Masahiro Kanazaki

  13. Effective Operations of Extinction-Reignition with Simple Control of Oxidizer Flux on a Single-Stage Sounding Hybrid Rocket

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

    Dr Masahiro Kanazaki, Dr. Toru Shimada, Kazuhisa Chiba

  14. Trajectory and Aerodynamic Control Optimization of Civil Aircraft Descent Under Hazard Situations Based on High-Fidelity Aerodynamic Database

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

    Dr Masahiro Kanazaki

  15. Influence of Engine Intake/Exhaust on Wing Design of Civil Aircraft by Means of Knowledge Discovery Techniques

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

    Dr Masahiro Kanazaki, Kazuomi Yamamoto

  16. Ascendancy of Extinction-Reignition on Single-Stage Hybrid Sounding Rocket in View of Fuels

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

    Dr Masahiro Kanazaki, Dr. Toru Shimada, Koki Kitagawa, Kazuhisa Chiba

  17. Efficient Flight Simulation Using Kriging Surrogate Model Based Aerodynamic Database

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

    Mrs Norazila Othman, Dr Masahiro Kanazaki

  18. Efficient global optimization applied to wind tunnel evaluation-based optimization for improvement of flow control by plasma actuators

    Article • Engineering Optimization, September 2014, Taylor & Francis

    Dr Masahiro Kanazaki, Dr Takashi Matsuno

  19. Unsteady Numerical Simulations of HTV-R Reentry Capsule by Using Detached-Eddy Simulation

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

    Dr Masahiro Kanazaki, Takashi Aoyama