Actuator concepts for active gust alleviation on transport aircraft at transonic speeds
Author:
Affiliation:
1. Technical University of Braunschweig
2. University of Stuttgart
3. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Reference25 articles.
1. Active Flutter Suppression-A Flight Test Demonstration
2. Prediction of gust loadings and alleviation at transonic speeds
3. Experimental measurements of dynamic control surface effectiveness
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4. Conventional and Unconventional Control Effectors for Load Alleviation in High-Aspect-Ratio-Wing Aircraft;AIAA SCITECH 2022 Forum;2022-01-03
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