Method for Evaluating Electrically Actuated Hybrid Wing–Body Control Surface Layouts
Author:
Affiliation:
1. Aerospace Systems Design Laboratory, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033061
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