High-accuracy large-step explicit Runge-Kutta (HALE-RK) schemes for computational aeroacoustics
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Publication:1025140
DOI10.1016/j.jcp.2009.02.015zbMath1171.76039OpenAlexW1980565389MaRDI QIDQ1025140
M. Nallasamy, Vasanth Allampalli, Scott D. Sawyer, Ray Hixon
Publication date: 18 June 2009
Published in: Journal of Computational Physics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jcp.2009.02.015
Finite difference methods applied to problems in fluid mechanics (76M20) Hydro- and aero-acoustics (76Q05)
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Cites Work
- Unnamed Item
- Dispersion-relation-preserving finite differene schemes for computational acoustics
- A new minimum storage Runge-Kutta scheme for computational acoustics
- Low-storage Runge-Kutta schemes
- Compact finite difference schemes with spectral-like resolution
- \(2N\)-storage low dissipation and dispersion Runge-Kutta schemes for computational acoustics
- Several new numerical methods for compressible shear-layer simulations
- Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics
- VERY HIGH-ORDER SPATIALLY IMPLICIT SCHEMES FOR COMPUTATIONAL ACOUSTICS ON CURVILINEAR MESHES
- Optimized compact finite difference schemes with maximum resolution
- Computational aeroacoustics - Issues and methods
