A block interface flux reconstruction method for numerical simulation with high order finite difference scheme

DOI10.1016/j.jcp.2012.12.037zbMath1349.76463OpenAlexW2043645601MaRDI QIDQ346330

Junhui Gao

Publication date: 5 December 2016

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jcp.2012.12.037

zbMATH Keywords

stabilitycomputational aeroacousticshigh order finite difference methodinterface flux reconstructionoverlap grid

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20)

Related Items (3)

An efficient meshfree point collocation moving least squares method to solve the interface problems with nonhomogeneous jump conditions ⋮ A new family of weighted one-parameter flux reconstruction schemes ⋮ An overset grid method for large eddy simulation of turbomachinery stages

Uses Software

• PEGASUS 5

Cites Work

• Unnamed Item
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• Spectral difference method for unstructured grids. II. Extension to the Euler equations
• Sound generation by a two-dimensional circular cylinder in a uniform flow
• Computational aeroacoustics - Issues and methods
• Computational Aeroacoustics: An Overview of Computational Challenges and Applications
• COMPUTATIONAL PREDICTION OF FLOW-GENERATED SOUND

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