All Stories

  1. Trailing-Edge Bluntness Noise Attenuation Using Spanwise Varying Porosity
  2. Airfoil Noise Reduction Produced by Leading Edge Serrations
  3. Reduction of Leading-Edge Noise by Tailored Turbulence Anisotropy
  4. The Effect of Pressure Gradient on the Aeroacoustics and Wake Dynamics of a Finite Wall-Mounted Square Cylinder
  5. Wing Tip Vortex Formation Noise
  6. Schlieren Image Velocimetry for Wall-Bounded Supersonic Flows
  7. Unsteady Interaction between Shear Layer Vortices and a Bow Shock During Supersonic Injection
  8. Transient Aspects of a Shock-Wave Boundary Layer Interaction
  9. Two-step hybrid calibration of remote microphones
  10. Novel techniques to enhance the focal-resolution and characterization of experimental flow-induced dipole sources using time-reversal
  11. Unsteady Flow Physics of the Blade-Tower Interaction of a Pylon-Mounted Fan
  12. A Microphone Array Method Benchmarking Exercise using Synthesized Input Data
  13. A Comparison of Microphone Phased Array Methods Applied to the Study of Airframe Noise in Wind Tunnel Testing
  14. Camber Effects on the Tonal Noise and Flow Characteristics of a Wall-mounted Finite Airfoil
  15. Characterisation and modelling of axial fan noise
  16. An empirical de-reverberation technique for closed-section wind tunnel beamforming
  17. An Investigation of the Tonal Noise Produced by a Wall-mounted Finite Airfoil at Angle of Attack
  18. Airfoil noise production and prediction
  19. Computational Methodology for Investigating the Transient Interaction Between a Reaction Control Jet and a Hypersonic Crossflow
  20. Experimental Application of Aeroacoustic Time-Reversal
  21. Enhancing the Resolution Characteristics of Aeroacoustic Time-Reversal Using a Point-Time-Reversal-Sponge-Layer
  22. An Experimental Comparison of Beamforming, Time-reversal and Near-field Acoustic holography for Aeroacoustic Source Localization
  23. Flow modelling and noise generation of interacting prisms
  24. An Experimental Study of the Flow-induced Noise Created by a Wall-mounted Finite Length Airfoil