Multibody Dynamic Modeling and Simulation of a Tailless Folding Wing Morphing Aircraft
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics
2. The First Aircraft Institute of AVIC-I
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6155
Reference6 articles.
1. Benefits and design challenges of adaptive structures for morphing aircraft
2. 25, No.3, 1988,pp.216-221.
3. Journal of Aircraft, Vol. 44, No.4, 2007, pp1077-1087.
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