Affiliation:
1. University of Maryland
Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. 1Bolonkin, A., Gilyard, G.B. "Estimated Benefits of Variable-Geometry Wing Camber Control for Transport Aircraft," NASA TechnicalMemorandum, NASA/TM-1999-206586.
2. Drag Reduction Methodology for Adaptive Tailless Aircraft
3. Ideal Lift Distributions and Flap Angles for Adaptive Wings
4. Simulation to Flight Test for a UAV Controls Testbed
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2 articles.
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