Transition on swept leading edges at Mach 3.5
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45511
Reference18 articles.
1. On the Flow Along Swept Leading Edges
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