Method for Enhancement of the Rolling Maneuver of a Flexible Wing
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433
2. University of Dayton, Dayton, Ohio 45469
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2228
Reference11 articles.
1. An active flexible wing multi-disciplinary design optimization method
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1. Optimal Rolling Maneuvers with Very Flexible Wings;AIAA Journal;2017-09
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3. Flight Dynamics of Morphing Aircraft with Time-Varying Inertias;Morphing Aerospace Vehicles and Structures;2012-03-14
4. Effects of Time-Varying Inertias on Flight Dynamics of an Asymmetric Variable-Sweep Morphing Aircraft;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2007-06-15
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