Micro Air Vehicle Scale Gust-Wing Interaction in a Wind Tunnel
Author:
Affiliation:
1. University of Maryland, College Park
2. Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0573
Reference13 articles.
1. 1Donely, P., Summary of Information Relating to Gust Loads on Airplanes, NACA Report 997, 1950.
2. 5Theodorsen, T., General theory of aerodynamic instability and the Mechanism of Flutter, NACA Report 496, 1935.
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