Flow control device evaluation for an internal flow with an adverse pressure gradient
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-266
Reference59 articles.
1. Some Thoughts on the Design of Subsonic Transport Aircraft for the 21st Century
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