Euler solver for three-dimensional supersonic flows with subsonic pockets
Author:
Affiliation:
1. Rockwell International Science Center, Thousand Oaks, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45423
Reference10 articles.
1. Nonlinear computation of wing-body-vertical tail-wake flows at low supersonic speeds
2. Numerical issues in computing inviscid supersonic flow over conical delta wings
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