All Stories

  1. Ground Effects on Mach Cutoff Phenomena of Sonic Boom

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

    Yoshikazu Makino

  2. Modified Methods to Estimate Atmospheric Turbulent Scales in Various Altitudes and Climatological Conditions

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

    Yoshikazu Makino

  3. Sensitivity Study and Primary Boom Carpet Assessment for Conceptual Low Boom Supersonic Transport

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

    Yoshikazu Makino

  4. Near Field Sonic Boom Simulations for C608 airplane of the Third AIAA SPW by Unstructured/Structured Overset Grid Method

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

    Yoshikazu Makino

  5. Numerical Evaluation of Sonic Boom Deformation due to Atmospheric Turbulence

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

    Yoshikazu Makino

  6. Statistical Characterization of Atmospheric Turbulent Scales in Hot-Dry and Hot-Humid Climates

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

    Yoshikazu Makino, Dr. Tatsunori Yuhara

  7. Sonic Boom Assessment in Primary Boom Carpet of Low-Boom Supersonic Airplane (NASA C25D)

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

    Yoshikazu Makino

  8. Extension of Multipole Analysis to Laterally Asymmetric Flowfield Around Supersonic Flight Vehicle

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

    Yoshikazu Makino

  9. Comparison of Simulated Sonic Boom in Stratified Atmosphere with Flight Test Measurements

    Article • AIAA Journal, July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Yoshikazu Makino

  10. Statistical Characterization of Atmospheric Turbulence Behavior Responsible for Sonic Boom Waveform Deformation

    Article • AIAA Journal, February 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Yoshikazu Makino

  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. Effect of Low-Boom Waveform on Focus Boom Using Lossy Nonlinear Tricomi Analysis

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

    Yoshikazu Makino

  13. Effects of Uncertainties in Atmospheric Turbulence and Weather Predictions on Sonic Boom

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

    Yoshikazu Makino

  14. Characteristic Scales of Atmospheric Turbulence Responsible for Sonic Boom Propagation

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

    Yoshikazu Makino

  15. Numerical Evauation of Effect of Atmospheric Turbulence on Sonic Boom Observed in D-SEND#2 Flight Test

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

    Yoshikazu Makino

  16. Robust Low-Boom Design Based on Near-Field Pressure Signature in Whole Boom Carpet

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

    Yoshikazu Makino

  17. Conceptual Design Study on Liquid Hydrogen-Fueled Supersonic Transport Considering Environmental Impacts

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

    Prof Kenichi Rinoie, Dr. Tatsunori Yuhara, Yoshikazu Makino

  18. Multi-fidelity Low-boom Design Based on Near-field Pressure Signature

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

    Yoshikazu Makino

  19. Conceptual Design Study on LH2 Fueled Supersonic Transport considering Performance and Environmental Impacts

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

    Prof Kenichi Rinoie, Yoshikazu Makino