Optimization of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Bristol, Bristol, England BS8 1TR, United Kingdom
2. Airbus Operations Ltd., Bristol, England BS99 7AR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053599
Reference43 articles.
1. Aeroelastic Tailoring of Forward Swept Composite Wings
2. Aeroelastic tailoring - Theory, practice, and promise
3. Aeroelastic Tailoring of Composite Structures
4. Induced Drag Reduction Using Aeroelastic Tailoring with Adaptive Control Surfaces
5. Optimization of a Wing Structure for Gust Response and Aileron Effectiveness
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