Aerostructural design optimization of a continuous morphing trailing edge aircraft for improved mission performance
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3209
Reference29 articles.
1. Design and application of compliant mechanisms for morphing aircraft structures
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