Hybrid Discontinuous Galerkin and Finite Volume Method for Launch Environment Acoustics Prediction
Author:
Affiliation:
1. Aerospace and Defense Division, CFD Research Corporation, Huntsville, Alabama 35806
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053877
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