Fast, Unstructured-Mesh Finite-Element Method for Nonlinear Subsonic Flow
Author:
Affiliation:
1. Royal Institute of Technology, 100 44 Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031738
Reference28 articles.
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