Design and Trajectory Optimization of a Morphing Wing Aircraft
Author:
Affiliation:
1. University of Michigan, Ann Arbor
2. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1382
Reference33 articles.
1. Mission Adaptive Wing System for Tactical Aircraft
2. Variable wing camber for transport aircraft
3. AFTI/F-111 Mission Adaptive Wing flight research program
4. Design and application of compliant mechanisms for morphing aircraft structures
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