Active Gust Load Alleviation by Combined Actuation of Trailing Edge and Leading Edge Flap at Transonic Speeds
Author:
Affiliation:
1. University of Stuttgart
2. Technical University of Braunschweig
3. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Reference29 articles.
1. Aircraft Design with Active Load Alleviation and Natural Laminar Flow
2. Model-Predictive Gust Load Alleviation Controller for a Highly Flexible Aircraft
3. Gust Loads Alleviation Using Special Control Surfaces
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