A set of explicit finite difference schemes with large stencil was optimized to obtain maximum resolution characteristics for various spatial truncation orders. The effect of integral interval range of the objective function on the optimized schemes’ performance is discussed. An algorithm is developed for the automatic determination of this integral interval. Three types of objective functions in the optimization procedure are compared in detail, which show that Tam’s objective function gets the best resolution in explicit centered finite difference scheme. Actual performances of the proposed optimized schemes are demonstrated by numerical simulation of three CAA benchmark problems. The effective accuracy, strengths, and weakness of these p...
Computational aeroacoustics requires efficient, high-resolution simulation tools. And for smooth pro...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
Computational aeroacoustics requires numerical techniques capable of yielding low artificial dispers...
A set of optimised boundary closure schemes is presented for use with compact central finite differe...
Direct numerical simulations and computational aeroacoustics require an accurate finite difference s...
The numerical simulation of aeroacoustic phenomena requires high-order accurate numerical schemes wi...
A variety of aeroacoustic problems involve small-amplitude linear wave propagation. Highorder scheme...
The performances of high-order, highly efficient finite difference schemes with Runge-Kutta time int...
In this paper, we have combined some spatial derivatives with the optimised time derivative proposed...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...
This paper compares the performance of two optimized high-order finite-difference schemes with Runge...
The numerical simulation of aeroacoustic phenomena requires high-order accurate numerical schemes wi...
In this work a patched grid technique is proposed with the aim of increasing the flexi-bility and ef...
The optimized high-order Dispersion-Relation-Preserving finite difference scheme is extended so as t...
In the implementation of spectral difference (SD) method, the conserved variables at the flux points...
Computational aeroacoustics requires efficient, high-resolution simulation tools. And for smooth pro...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
Computational aeroacoustics requires numerical techniques capable of yielding low artificial dispers...
A set of optimised boundary closure schemes is presented for use with compact central finite differe...
Direct numerical simulations and computational aeroacoustics require an accurate finite difference s...
The numerical simulation of aeroacoustic phenomena requires high-order accurate numerical schemes wi...
A variety of aeroacoustic problems involve small-amplitude linear wave propagation. Highorder scheme...
The performances of high-order, highly efficient finite difference schemes with Runge-Kutta time int...
In this paper, we have combined some spatial derivatives with the optimised time derivative proposed...
Abstract: The main purpose of this work is the evaluation of spatial schemes used on CAA (Computatio...
This paper compares the performance of two optimized high-order finite-difference schemes with Runge...
The numerical simulation of aeroacoustic phenomena requires high-order accurate numerical schemes wi...
In this work a patched grid technique is proposed with the aim of increasing the flexi-bility and ef...
The optimized high-order Dispersion-Relation-Preserving finite difference scheme is extended so as t...
In the implementation of spectral difference (SD) method, the conserved variables at the flux points...
Computational aeroacoustics requires efficient, high-resolution simulation tools. And for smooth pro...
Since the earliest stages in computational aeroacoustics (CAA), the need for highly accurate schemes...
Computational aeroacoustics requires numerical techniques capable of yielding low artificial dispers...