Computational Modeling of Roughness-Based Laminar Flow Control on a Subsonic Swept Wing
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050503
Reference24 articles.
1. Leading-edge roughness as a transition control mechanism
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