Two problems are considered. Problem 1: Aeolian tones, sound generation by flow over cylinders, are relevant to airframe and power plant noise (heat exchanger, power transmission lines and chimneys). The purpose of this problem is to test the ability of a CFD/CAA code to accurately predict sound generation by viscous flows and sound propagation through interactions between acoustic wave & solid wall and between acoustic waves & shear layers. Problem 2: Sound generation by flow over a cavity.Air flows over the cavity shown below with a mean approach flow velocity of 50 m/s. The boundary layer that develops over the flat plate is turbulent with a thickness of 14 mm at the entrance to the cavity. Calculate the power spectra at the center of ea...
This thesis investigates the use of Computational Aeroacoustics (CAA) in predicting sound generation...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
Solve the time-dependent inviscid flow equations for this geometry subject to the specified inflow/o...
Three benchmark problems from the current and previous CAA workshops involving tone noise generated ...
A large variety of hybrid computational aeroacoustics (CAA) approaches exist differing from each oth...
Computational approaches are being developed to study a range of problems in aeroacoustics. These ae...
Computational approaches are being developed to study a range of problems in aeroacoustics. These ae...
The Computational Aeroacoustics (CAA) Workshops on Benchmark Problems have been organized to gauge t...
A novel linearised Navier-Stokes equations method including turbulence information is developed to s...
Computational Aeroacoustics (CAA) is the coupling of solving the flow field using numerical method a...
Aeroengine noise is one of the dominating noise sources in today’s aircraft. Reduction of the aeroen...
Since the direct numerical simulation (DNS) of aeroacoustic noise requires the numerical solution of...
Aeroengine noise is one of the dominating noise sources in today’s aircraft. Reduction of the aeroen...
Numerical simulations of the sound generation by flow over surface mounted cylindrical cavities incl...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
This thesis investigates the use of Computational Aeroacoustics (CAA) in predicting sound generation...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
Solve the time-dependent inviscid flow equations for this geometry subject to the specified inflow/o...
Three benchmark problems from the current and previous CAA workshops involving tone noise generated ...
A large variety of hybrid computational aeroacoustics (CAA) approaches exist differing from each oth...
Computational approaches are being developed to study a range of problems in aeroacoustics. These ae...
Computational approaches are being developed to study a range of problems in aeroacoustics. These ae...
The Computational Aeroacoustics (CAA) Workshops on Benchmark Problems have been organized to gauge t...
A novel linearised Navier-Stokes equations method including turbulence information is developed to s...
Computational Aeroacoustics (CAA) is the coupling of solving the flow field using numerical method a...
Aeroengine noise is one of the dominating noise sources in today’s aircraft. Reduction of the aeroen...
Since the direct numerical simulation (DNS) of aeroacoustic noise requires the numerical solution of...
Aeroengine noise is one of the dominating noise sources in today’s aircraft. Reduction of the aeroen...
Numerical simulations of the sound generation by flow over surface mounted cylindrical cavities incl...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
This thesis investigates the use of Computational Aeroacoustics (CAA) in predicting sound generation...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
Solve the time-dependent inviscid flow equations for this geometry subject to the specified inflow/o...