Evaluation of boundary conditions for computational aeroacoustics
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12940
Reference12 articles.
1. Structure of supersonic jet flow and its radiated sound
2. Time dependent boundary conditions for hyperbolic systems
3. Time-dependent boundary conditions for hyperbolic systems, II
4. Nonreflecting boundary conditions for Euler equation calculations
5. Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics
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