Most computational fluid dynamics (CFD) schemes are not adequately accurate for solving aeroacoustics problems, which have wave amplitudes several orders of magnitude smaller yet with frequencies larger than the flow field variations generating the sound. Hence, a computational aeroacoustics (CAA) algorithm should have minimal dispersion and dissipation features. A dispersion relation preserving (DRP) scheme is, therefore, applied to solve the linearized Euler equations in order to simulate the propagation of three types of waves, namely: acoustic, vorticity, and entropy waves. The scheme is derived using an optimization procedure to ensure that the numerical derivatives preserve the wave number and angular frequency of the partial differen...
The main purpose of this work is the evaluation of the interaction of the spatial schemes (Tradition...
Higher order compact algorithms are developed for the numerical simulation of wave propagation by us...
The scientific committee, after careful consideration, adopted six categories of benchmark problems ...
Important characteristics of the aeroacoustic wave propagation are mostly encoded in their dispersio...
As a review framework, the present study describes the application and performance of different nume...
Computational aeroacoustics often use finite difference schemes optimized to require relatively few ...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...
Computational approaches are being developed to study a range of problems in aeroacoustics. These ae...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
This thesis presents a method for computational aeroacoustics, primarily aimed at computing sound pr...
The present paper investigates the numerical methods used to predict aerodynamically generated noise...
The direct simulation of sound sources and sound fields in flows is a rapidly growing area in resear...
The aeroacoustics of rigid boundaries is discussed. Lighthill gave a formulation of this problem in ...
We present a study of the effect of artificial dissipation models on nonlinear wave computations usi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76586/1/AIAA-1993-3382-851.pd
The main purpose of this work is the evaluation of the interaction of the spatial schemes (Tradition...
Higher order compact algorithms are developed for the numerical simulation of wave propagation by us...
The scientific committee, after careful consideration, adopted six categories of benchmark problems ...
Important characteristics of the aeroacoustic wave propagation are mostly encoded in their dispersio...
As a review framework, the present study describes the application and performance of different nume...
Computational aeroacoustics often use finite difference schemes optimized to require relatively few ...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...
Computational approaches are being developed to study a range of problems in aeroacoustics. These ae...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
This thesis presents a method for computational aeroacoustics, primarily aimed at computing sound pr...
The present paper investigates the numerical methods used to predict aerodynamically generated noise...
The direct simulation of sound sources and sound fields in flows is a rapidly growing area in resear...
The aeroacoustics of rigid boundaries is discussed. Lighthill gave a formulation of this problem in ...
We present a study of the effect of artificial dissipation models on nonlinear wave computations usi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76586/1/AIAA-1993-3382-851.pd
The main purpose of this work is the evaluation of the interaction of the spatial schemes (Tradition...
Higher order compact algorithms are developed for the numerical simulation of wave propagation by us...
The scientific committee, after careful consideration, adopted six categories of benchmark problems ...