Transient behavior of supersonic flow through inlets
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, Ohio 45221
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10976
Reference22 articles.
1. RNS/Euler pressure relaxation and flux vector splitting
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3. A local grid refinement procedure through segmented multigrid domain decomposition for three dimensional flows;12th Computational Fluid Dynamics Conference;1995-06-19
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