System Benefits of Active Flutter Suppression for a SensorCraft-Type Vehicle
Author:
Affiliation:
1. Lockheed Martin Corporation
2. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-9349
Reference13 articles.
1. 1Hunten, K.A., Zink, S., Flansburg, B., and Englestad, S. "A Systems MDO Approach for an Unmanned Aerial Vehicle," AIAA-2007-1877.
2. 3Zink, S., Love, M., and Youngren, H. "Drag Minimization Through the use of Mission Adaptive Trailing Edge Flaps and Fuel StateControl,"AIAA-2004-4365.
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