Flight Dynamics of Transport Aircraft Equipped with Flared-Hinge Folding Wingtips
Author:
Affiliation:
1. Khalifa University of Science and Technology, Abu Dhabi, United Arab Emirates
Funder
Abu Dhabi Education Council (ADEK) Award for Research Excellent Program
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference18 articles.
1. Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation
2. Nonlinear Folding Wing Tips for Gust Loads Alleviation
3. Nonlinear Negative Stiffness Wingtip Spring Device for Gust Loads Alleviation
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