Abstract. In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen and Sørensen1, will be used and discussed for the simulation of flow-induced sound at low Mach numbers. The method consists of two parts: First solving for the incompressible, viscous flow field, and second computing the fluctuating acoustic field. As a result of this splitting approach, one can choose optimized numerical methods and grid sizes for each of the two parts. In the current contribution an explicit finite difference scheme is employed to solve the nonlinear acoustic equations, and the propagation and scattering of the sound are computed simultaneously. The acoustic results are presented for the sound generated by a circular cylin...
This work proposes to address the computation of flow-generated noise, including the high frequency ...
The flow-generated sound from cylinders with different cross-sections have been investigated using l...
The computation of flow-induced noise at low Mach numbers usually relies on a two-step hybrid method...
In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen and Søren...
In many practical applications, sound is generated by interaction of turbulent flow with solid objec...
The objective of this paper is to calculate the far-field sound generated from low mach number flow ...
This contribution deals with the acoustic simulation of aerodynamical noise generated by a flow over...
Hybrid computational aeroacoustics applications approaches, in which the computational domain is spl...
The hybrid aeroacoustic approach is an efficient way to address the issue of the disparity of scales...
The sound generated by the flow around a circular cylinder is numerically investigated by using a fi...
An integrated hybrid approach for the numerical simulation of aeroacoustics at low Mach numbers is p...
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. The flow-...
The Expansion about Incompressible Flow (EIF) approach is a computational aeroacoustics (CAA) techni...
The Lighthill acoustic analogy approach combined with Reynolds�averaged Navier Stokes is used to pre...
In this paper, a hybrid computational aero/hydro-acoustic approach is proposed to deal with acoustic...
This work proposes to address the computation of flow-generated noise, including the high frequency ...
The flow-generated sound from cylinders with different cross-sections have been investigated using l...
The computation of flow-induced noise at low Mach numbers usually relies on a two-step hybrid method...
In the present paper an Expansion about Incompressible Flow approach, as suggested by Shen and Søren...
In many practical applications, sound is generated by interaction of turbulent flow with solid objec...
The objective of this paper is to calculate the far-field sound generated from low mach number flow ...
This contribution deals with the acoustic simulation of aerodynamical noise generated by a flow over...
Hybrid computational aeroacoustics applications approaches, in which the computational domain is spl...
The hybrid aeroacoustic approach is an efficient way to address the issue of the disparity of scales...
The sound generated by the flow around a circular cylinder is numerically investigated by using a fi...
An integrated hybrid approach for the numerical simulation of aeroacoustics at low Mach numbers is p...
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. The flow-...
The Expansion about Incompressible Flow (EIF) approach is a computational aeroacoustics (CAA) techni...
The Lighthill acoustic analogy approach combined with Reynolds�averaged Navier Stokes is used to pre...
In this paper, a hybrid computational aero/hydro-acoustic approach is proposed to deal with acoustic...
This work proposes to address the computation of flow-generated noise, including the high frequency ...
The flow-generated sound from cylinders with different cross-sections have been investigated using l...
The computation of flow-induced noise at low Mach numbers usually relies on a two-step hybrid method...