Grid-optimized upwind DRP finite difference scheme on curvilinear grids for computational aeroacoustics
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference13 articles.
1. Grid-optimized dispersion-relation-preserving schemes on general geometries for computational aeroacoustics;Cheong;Journal of Computational Physics,2001
2. Aeroacoustic computational using a high-order shock-capturing scheme;Daru;AIAA Journal,2007
3. Aeroacoustic predictions using high-order shock-capturing schemes;Ekaterinaris;International Journal of Aeroacoustics,2003
4. Stream function–potential function coordinates for aeroacoustics and unsteady aerodynamics;Gopalan;International Journal of Computational Fluid Dynamics,2009
5. A stable perfectly matched layer for linearized Euler equations in unsplit physical variables;Hu;Journal of Computational Physics,2001
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1. Optimized compact finite volume formulation with dispersion relation preserving characteristics in structured space discretizations;International Journal of Aeroacoustics;2024-05-30
2. Grid transformation and dynamic scattering for tail rotor radar cross section analysis;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-10-21
3. Effect of non-uniform mean flow field on acoustic propagation problems in computational aeroacoustics;Aerospace Science and Technology;2013-07
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