Effects of splitter plates on the wake flow behind a bluff body
Author:
Affiliation:
1. Hewlett Packard, Cupertino, California
2. Queen's University, Kingston, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.25119
Reference17 articles.
1. Experiments on the flow past a circular cylinder at very high Reynolds number
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