Drag Reduction Methodology for Adaptive Tailless Aircraft
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695-7910
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031454
Reference30 articles.
1. Ideal Lift Distributions and Flap Angles for Adaptive Wings
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