An Overview of High-Order Finite Difference Schemes for Computational Aeroacoustics (original) (raw)

A Numerical Validation of a High-Order Finite-Difference Compact Scheme for Computational Aeroacoustics

Christophe Airiau

46th AIAA Aerospace Sciences Meeting and Exhibit, 2008

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Comparison of Optimized High-Order Finite-Difference Schemes for Computational Aeroacoustics

Aldo Rona

47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, 2009

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A selective overview of high-order finite-difference schemes for aeroacoustic applications

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An overview of some high order and multi-level finite difference schemes in computational aeroacoustics

Muhammad Dauhoo

Proceedings of World Academy of Science, …, 2009

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Investigation of high-order cell-centered finite difference method for aeroacoustics

Philip Morris

25th AIAA/CEAS Aeroacoustics Conference, 2019

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Second-Order Accuracy in Time of Finite Difference Methods for Computational Aeroacoustics

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Jurnal Kejuruteraan, 2023

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Multidimensional optimization of finite difference schemes for Computational Aeroacoustics

Abdollah Afjeh

Journal of Computational Physics, 2008

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Wall boundary conditions for high-order finite-difference schemes in computational aeroacoustics

Prasanth Kutchu

Theoretical and Computational Fluid Dynamics, 1994

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Implementation of a High-Order Finite Difference Scheme to Model Wave Propagation

Aldo Rona

13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), 2007

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A numerical validation of a high-order flnite-difierence compact scheme for computational aeroacoustics

Christophe Airiau, Aldo Rona

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Advances in computational aeroacoustics: challenges and issues

Olivier Marsden

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The Technique of MIEELDLD in Computational Aeroacoustics

Rao Appadu

Journal of Applied Mathematics, 2012

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High Order Methods with Applications to Aerodynamics and Aeroacoustics

Joao Luiz F Azevedo

2015

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ICASE/LaRC Workshop on Benchmark Problems in Computational Aeroacoustics (CAA)

ray Ristorcelli

1995

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Computational aeroacoustics: issues and methods

Prasanth Kutchu

AIAA journal, 1995

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A High-Order Immersed Boundary Technique for Computational Aeroacoustics

Christian Prax

HAL (Le Centre pour la Communication Scientifique Directe), 2022

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Highly stable RK time advancing schemes for Computational Aero Acoustics

M. Calvo, L. Rández

SeMA Journal, 2010

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Computational aeroacoustics: progress on nonlinear problems of sound generation

Prasanth Kutchu

Progress in Aerospace Sciences, 2004

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A Sixth-Order Compact Finite-Volume Scheme for Aeroacoustics: Application to a Large Eddy Simulation of a Jet

Hugues Deniau

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High-accuracy large-step explicit Runge–Kutta (HALE-RK) schemes for computational aeroacoustics

Scott Sawyer

Journal of Computational Physics, 2009

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Finite element hybrid and direct computational aeroacoustics at low Mach numbers in slow time-dependent domains

Oriol Guasch

Computers & Fluids, 2022

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Grid-optimized upwind DRP finite difference scheme on curvilinear grids for computational aeroacoustics

Du Chen

Aerospace Science and Technology, 2011

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The perturbed low Mach number approximation for the aeroacoustic computation of anisothermal flows

Cyril Nana

HAL (Le Centre pour la Communication Scientifique Directe), 2012

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An Improved Family of Low Dispersion Finite Volume Schemes for Aeroacoustic Applications

Lakshmi Sankar

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Application of an Accuracy Enhancing Post-Processing Method to Aeroacoustic Simulations

Jennifer K Ryan, H. Atkins, Chi-wang Shu

9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003

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Computational and asymptotic methods in aeroacoustics with applications

Rustem Aslan

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Computing Aerodynamically Generated Noise

Rosemary Renaut

Annual Review of Fluid Mechanics, 1997

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High-Fidelity Computational Aeroacoustics Through CE/SE Based Transient Viscous Solver

Gary Cheng

46th AIAA Aerospace Sciences Meeting and Exhibit, 2008

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The Influence of Flow Domain Modeling on the Accuracy of Direct and Hybrid Aeroacoustic Noise Calculations

Wim Desmet, W. De Roeck

12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), 2006

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Toward a high-order preserving sliding-mesh approach for computational aeroacoustics in subsonic turbomachinery

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