All Stories

  1. Noise Prediction of NASA CRM-HL Using Lattice-Boltzmann Method and Wall-Modeled LES

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Kazuomi Yamamoto

  2. Computational Study on Track Noise From Infinite Wing with Leading-Edge Krueger Flap

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Kazuomi Yamamoto

  3. Computational Study of Noise Characteristics From 30P30N Leading-Edge Slat and Krueger Flap

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

    Kazuomi Yamamoto, Dr. Meelan Choudhari

  4. Landing Gear Noise Reduction Using Porous Plates

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

    Kazuomi Yamamoto

  5. Computational Study on Porous-Plates for Reducing Airframe Noise Associated With Landing Gear Bay

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

    Kazuomi Yamamoto

  6. Experimental and Numerical Investigation on Noise Directivity of the 30P30N Three-Element High-Lift Airfoil

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

    Kazuomi Yamamoto

  7. Noise Reduction Design for High Lift Devices of Regional Jet

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

    Kazuomi Yamamoto

  8. Slat Noise Reduction Based on Turbulence Attenuation Downstream of Shear-layer Reattachment

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

    Kazuomi Yamamoto

  9. Effect of Slat Tracks and Inboard Slat Tip Geometry on Airframe Noise

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

    Kazuomi Yamamoto

  10. Computational Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin

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

    Dr. Shunsuke Koike, Kazuomi Yamamoto, Kazuhiro Kusunose

  11. JAXA’s and KHI’s Contribution to the Third High Lift Prediction Workshop

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

    Kazuomi Yamamoto, Atsushi Tajima

  12. Wind Tunnel Interference Effects on Japan Aerospace Exploration Agency’s Standard Model

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

    Kazuomi Yamamoto

  13. Flap Surface Pressure Measurements with 3D printed Pressure Belts in FQUROH Flight Demonstration

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

    Kazuomi Yamamoto, Hideo Omotani

  14. Numerical Simulation of Main Landing Gear Noise Reduction in FQUROH Flight Demonstration

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

    Kazuomi Yamamoto

  15. Lattice-Boltzmann Simulations of the JAXA JSM High-Lift Configuration in a Wind Tunnel

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

    Kazuomi Yamamoto

  16. FQUROH: A Flight Demonstration Project for Airframe Noise Reduction Technology – the 2nd Flight Demonstration

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

    Kazuomi Yamamoto

  17. Quadrupole Corrections for the Permeable-Surface Ffowcs Williams–Hawkings Equation

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

    Dr. Shunji ENOMOTO, Kazuhisa Amemiya, Kazuomi Yamamoto

  18. TAS Code, FaSTAR, and Cflow Results for the Sixth Drag Prediction Workshop

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

    Kazuomi Yamamoto, Takashi Aoyama

  19. Noise Reduction Design for Landing Gear toward FQUROH Flight Demonstration

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

    Kazuomi Yamamoto

  20. Acoustic Wind Tunnel Test with 18% scale Half-span Model toward FQUROH Flight Demonstration

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

    Kazuomi Yamamoto

  21. Noise Reduction Design for Flap Side-edges toward FQUROH Flight Demonstration

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

    Kazuomi Yamamoto

  22. Airframe Noise Reduction of Flap Side-edge Using Vortex Generators

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

    Kazuomi Yamamoto

  23. FQUROH: A Flight Demonstration Project for Airframe Noise Reduction Technology - the 1st Flight Demonstration

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

    Kazuomi Yamamoto

  24. High-Fidelity Aerodynamic Analysis of Aircraft in Various Configurations with MEGG3D

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

    Kazuomi Yamamoto

  25. TAS Code, FaSTAR and Cflow Results for the Sixth Drag Prediction Workshop

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

    Kazuomi Yamamoto, Takashi Aoyama

  26. Lattice-Boltzmann Simulations of the JAXA JSM High-Lift Configuration

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

    Kazuomi Yamamoto

  27. Study on Change of Noise Generation from Slat Track Shape

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

    Kazuomi Yamamoto

  28. The Frequency-Domain Formulations of the Quadrupole Correction for the Ffowcs Williams-Hawkings Integration

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

    Kazuhisa Amemiya, Kazuomi Yamamoto

  29. Lattice-Boltzmann Flow Simulation of a Two-Wheel Landing Gear

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

    Kazuomi Yamamoto

  30. Flyover Array Measurements with JAXA Flying Test Bed ‘Hisho’

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

    Kazuomi Yamamoto

  31. FQUROH: a Flight Demonstration Project for Airframe Noise Reduction Technology - Concept and Current Status

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

    Kazuomi Yamamoto

  32. 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

  33. Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop

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

    Kazuomi Yamamoto

  34. Automated Massively Refinement Technique for Multi-block Structured Grids Based on NURBS Volume

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

    Kazuomi Yamamoto

  35. Aeroacoustic Calculations of the 30P30N High-lift Airfoil using Hybrid RANS/LES methods: Modeling and Grid Resolution Effects

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

    Kazuomi Yamamoto

  36. Study on Noise Generation from Slat Tracks Using a High-Lift Wing Model

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

    Kazuomi Yamamoto

  37. Experimental Investigation of Vortex Generator Effect on Two- and Three-Dimensional NASA Common Research Models

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

    Dr. Shunsuke Koike, Kazuhiro Kusunose, Kazuomi Yamamoto

  38. Effect of Vortex Generators on Transonic Swept Wings

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

    Dr. Shunsuke Koike, Kazuhiro Kusunose, Kazuomi Yamamoto

  39. Japan Aerospace Exploration Agency Studies for the Fifth AIAA Drag Prediction Workshop

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

    Makoto Ueno, Kazuomi Yamamoto

  40. Experimental Study on Slat Noise from 30P30N Three-Element High-Lift Airfoil at JAXA Hard-Wall Lowspeed Wind Tunnel

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

    Dr. Meelan Choudhari, Kazuomi Yamamoto

  41. Summary of JAXA Studies for the 2nd AIAA CFD High Lift Prediction Workshop Using Structured and Unstructured Mesh CFD

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

    Kazuomi Yamamoto

  42. Experimental and Numerical Study of Jet Noise Reduction of HBPR Engine by Microjet Injection

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

    Dr. Shunji ENOMOTO, Kazuomi Yamamoto

  43. Turbulent Flow Solver Validation of FaSTAR and UPACS

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

    Kazuomi Yamamoto, Takashi Aoyama

  44. Towards Interference Corrections for Three-Dimensional Models in Kevlar-Walled Anechoic Test Sections

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

    Kazuomi Yamamoto