Interface Conditions of Finite Difference Compact Schemes for Computational Aeroacoustics
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.42110
Reference20 articles.
1. Pade-plusmn;-Type Higher-Order Boundary Filters for the Navier-Stokes Equations
2. Characteristic Interface Conditions for Multiblock High-Order Computation on Singular Structured Grid
3. Generalized characteristic interface conditions for high-order multi-block computation
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