Shear flow control by mechanical tabs
Author:
Affiliation:
1. Lockheed Aeronautical Systems Co., Marietta, GA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-994
Reference13 articles.
1. An experimental study of jet noise part II: Shock associated noise
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