Numerical Study of Novel Drag Reduction Techniques for Hypersonic Blunt Bodies

Title
Numerical Study of Novel Drag Reduction Techniques for Hypersonic Blunt Bodies
Authors
Keywords
-
Journal
AIAA JOURNAL
Volume 49, Issue 9, Pages 1871-1882
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2012-04-13
DOI
10.2514/1.j050681

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