A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field hydrodynamic disturbances in the turbulent boundary-layer scatter into radiated sound at small surface irregularities. In this paper, phased microphone arrays are applied to the measurement and simulation of surface roughness noise. The radiated sound from two rough plates and one smooth plate in an open jet is measured at three streamwise locations, and the beamforming source maps demonstrate the dipole directivity. Higher source strengths can be observed on the rough plates which also enhance the trailing-edge noise. A prediction scheme in previous theoretical work is used to describe the strength of a distribution of incoherent dipoles and ...
This thesis is concerned with the acoustic characterisation of flat plate aerofoils interacting with...
A small-aperture microphone phased array provides noise source maps for turbulent mixing noise emitt...
The turbulent flow over a porous trailing edge of a NACA 0018 airfoil is experimentally investigated...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field h...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field h...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field y...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field y...
Aircraft noise has been an increasing urgent environment issue especially for people living near air...
Aircraft noise has been an increasing urgent environment issue especially for people living near air...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary-layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary-layer flow at lowMach number over a rough wall is inve...
This thesis is concerned with the acoustic characterisation of flat plate aerofoils interacting with...
A small-aperture microphone phased array provides noise source maps for turbulent mixing noise emitt...
The turbulent flow over a porous trailing edge of a NACA 0018 airfoil is experimentally investigated...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field h...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field h...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field y...
A turbulent boundary-layer flow over a rough wall generates a dipole sound field as the near-field y...
Aircraft noise has been an increasing urgent environment issue especially for people living near air...
Aircraft noise has been an increasing urgent environment issue especially for people living near air...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary-layer flow at low Mach number over a rough wall is inv...
The generation of sound by turbulent boundary-layer flow at lowMach number over a rough wall is inve...
This thesis is concerned with the acoustic characterisation of flat plate aerofoils interacting with...
A small-aperture microphone phased array provides noise source maps for turbulent mixing noise emitt...
The turbulent flow over a porous trailing edge of a NACA 0018 airfoil is experimentally investigated...