Aeroelastic effects of spoiler surfaces on a low-aspect-ratio rectangular wing
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46244
Reference13 articles.
1. Aeroelastic oscillations caused by transitional boundary layers and their attenuation
2. Exploratory flutter test in a cryogenic wind tunnel
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