Add to ORKGA variety of aeroacoustic problems involve small-amplitude linear wave propagation. Highorder schemes have the accuracy and the low dispersion and dissipation wave propagation properties that are required to model linear acoustic waves with minimal spatial resolution. This review presents a selection of high-order finite difference time-explicit schemes for aeroacoustic applications. A scheme selection method based on the computational cost for a given accuracy level is proposed
A new family of prefactored cost-optimized schemes is developed to minimize the computational cost f...
A new class of cost-optimized prefactored high-order compact schemes, developed for shock-free error...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...
In this paper, we have combined some spatial derivatives with the optimised time derivative proposed...
aeroacoustics Abstract. This paper presents a short overview of recent developments of low-dispersiv...
This paper compares the performance of two optimized high-order finite-difference schemes with Runge...
This paper presents a short overview of recent developments of low-dispersive and low-dissipation fi...
Two families of finite difference algorithms for computational aeroacoustics are presented and compa...
The numerical simulation of aeroacoustic phenomena requires high-order accurate numerical schemes wi...
Computing sound directly from unsteady flows featuring large-scale instabilities requires numerical ...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
A set of explicit finite difference schemes with large stencil was optimized to obtain maximum resol...
Computational aeroacoustics often use finite difference schemes optimized to require relatively few ...
Direct numerical simulations and computational aeroacoustics require an accurate finite difference s...
This paper presents a review of high-order and optimized finite-difference methods for numerically s...
A new family of prefactored cost-optimized schemes is developed to minimize the computational cost f...
A new class of cost-optimized prefactored high-order compact schemes, developed for shock-free error...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...
In this paper, we have combined some spatial derivatives with the optimised time derivative proposed...
aeroacoustics Abstract. This paper presents a short overview of recent developments of low-dispersiv...
This paper compares the performance of two optimized high-order finite-difference schemes with Runge...
This paper presents a short overview of recent developments of low-dispersive and low-dissipation fi...
Two families of finite difference algorithms for computational aeroacoustics are presented and compa...
The numerical simulation of aeroacoustic phenomena requires high-order accurate numerical schemes wi...
Computing sound directly from unsteady flows featuring large-scale instabilities requires numerical ...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
A set of explicit finite difference schemes with large stencil was optimized to obtain maximum resol...
Computational aeroacoustics often use finite difference schemes optimized to require relatively few ...
Direct numerical simulations and computational aeroacoustics require an accurate finite difference s...
This paper presents a review of high-order and optimized finite-difference methods for numerically s...
A new family of prefactored cost-optimized schemes is developed to minimize the computational cost f...
A new class of cost-optimized prefactored high-order compact schemes, developed for shock-free error...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...