All Stories

  1. Computational Study of Noise Characteristics From 30P30N Leading-Edge Slat and Krueger Flap
  2. Landing Gear Noise Reduction Using Porous Plates
  3. Computational Study on Porous-Plates for Reducing Airframe Noise Associated With Landing Gear Bay
  4. Experimental and Numerical Investigation on Noise Directivity of the 30P30N Three-Element High-Lift Airfoil
  5. Noise Reduction Design for High Lift Devices of Regional Jet
  6. Slat Noise Reduction Based on Turbulence Attenuation Downstream of Shear-layer Reattachment
  7. Effect of Slat Tracks and Inboard Slat Tip Geometry on Airframe Noise
  8. Computational Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin
  9. JAXA’s and KHI’s Contribution to the Third High Lift Prediction Workshop
  10. Wind Tunnel Interference Effects on Japan Aerospace Exploration Agency’s Standard Model
  11. Flap Surface Pressure Measurements with 3D printed Pressure Belts in FQUROH Flight Demonstration
  12. Numerical Simulation of Main Landing Gear Noise Reduction in FQUROH Flight Demonstration
  13. Lattice-Boltzmann Simulations of the JAXA JSM High-Lift Configuration in a Wind Tunnel
  14. FQUROH: A Flight Demonstration Project for Airframe Noise Reduction Technology – the 2nd Flight Demonstration
  15. Quadrupole Corrections for the Permeable-Surface Ffowcs Williams–Hawkings Equation
  16. TAS Code, FaSTAR, and Cflow Results for the Sixth Drag Prediction Workshop
  17. Noise Reduction Design for Landing Gear toward FQUROH Flight Demonstration
  18. Acoustic Wind Tunnel Test with 18% scale Half-span Model toward FQUROH Flight Demonstration
  19. Noise Reduction Design for Flap Side-edges toward FQUROH Flight Demonstration
  20. Airframe Noise Reduction of Flap Side-edge Using Vortex Generators
  21. FQUROH: A Flight Demonstration Project for Airframe Noise Reduction Technology - the 1st Flight Demonstration
  22. High-Fidelity Aerodynamic Analysis of Aircraft in Various Configurations with MEGG3D
  23. TAS Code, FaSTAR and Cflow Results for the Sixth Drag Prediction Workshop
  24. Lattice-Boltzmann Simulations of the JAXA JSM High-Lift Configuration
  25. Study on Change of Noise Generation from Slat Track Shape
  26. The Frequency-Domain Formulations of the Quadrupole Correction for the Ffowcs Williams-Hawkings Integration
  27. Lattice-Boltzmann Flow Simulation of a Two-Wheel Landing Gear
  28. Flyover Array Measurements with JAXA Flying Test Bed ‘Hisho’
  29. FQUROH: a Flight Demonstration Project for Airframe Noise Reduction Technology - Concept and Current Status
  30. Influence of Engine Intake/Exhaust on Wing Design of Civil Aircraft by Means of Knowledge Discovery Techniques
  31. Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop
  32. Automated Massively Refinement Technique for Multi-block Structured Grids Based on NURBS Volume
  33. Aeroacoustic Calculations of the 30P30N High-lift Airfoil using Hybrid RANS/LES methods: Modeling and Grid Resolution Effects
  34. Study on Noise Generation from Slat Tracks Using a High-Lift Wing Model
  35. Experimental Investigation of Vortex Generator Effect on Two- and Three-Dimensional NASA Common Research Models
  36. Effect of Vortex Generators on Transonic Swept Wings
  37. Japan Aerospace Exploration Agency Studies for the Fifth AIAA Drag Prediction Workshop
  38. Experimental Study on Slat Noise from 30P30N Three-Element High-Lift Airfoil at JAXA Hard-Wall Lowspeed Wind Tunnel
  39. Summary of JAXA Studies for the 2nd AIAA CFD High Lift Prediction Workshop Using Structured and Unstructured Mesh CFD
  40. Experimental and Numerical Study of Jet Noise Reduction of HBPR Engine by Microjet Injection
  41. Turbulent Flow Solver Validation of FaSTAR and UPACS
  42. Towards Interference Corrections for Three-Dimensional Models in Kevlar-Walled Anechoic Test Sections