Aeroservoelastic Design Optimization of a Flexible Wing
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M5A 4L8, Canada
2. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031344
Reference51 articles.
1. Integrated aerodynamic/structural design of a sailplane wing
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5. Multidisciplinary Considerations in the Design of Wings and Wing Tip Devices
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