Towards an effective non-reflective boundary condition for computational aeroacoustics. (31st March 2017) - Gill, James
Abstract: A generic, non-reflective zonal transverse characteristic boundary condition is described for computational aeroacoustics, which shows superior performance to existing non-reflective boundary conditions for two-dimensional linearized Euler simulations. The new condition is based on a characteristic non-reflective method, and also contains optimised use of transverse characteristic terms and a zonal forcing region. The performance of the new method and several existing non-reflective acoustic boundary conditions is quantitatively compared using a plane wave test case. The performance of buffer zone, perfectly matched layer, far-field, and characteristic non-reflective methods is compared, following an optimisation of the tuneable parameters in each method to give best performance. The study uses a high-order linearised Euler equation solver to assess non-reflective boundary conditions with a variety of cases. The performance is compared for downstream travelling acoustic waves with varying frequency and incident angle, and at various Mach numbers. The current study includes a more comprehensive evaluation than previous studies which used constant values of tuneable parameters or qualitative assessment methods. The new zonal transverse characteristic boundary condition is shown to give improved performance in comparison to the other tested outflow boundary conditions for two-dimensional linearized Euler simulations, and is also shown to give good performance when used as an inflow condition. Abstract : Highlights: A variety of non-reflective boundary conditions are quantitatively evaluated. An improved zonal characteristic method is detailed and is shown to perform well. Buffer zone, PML, far-field, and characteristic methods are tested. Acoustic plane wave reflections are measured at various frequency, angle, and speeds. Zonal characteristic methods provide the best non-reflective performance. Testing is done for both outflow and inflow boundary conditions at a variety of Mach numbers.