Aeroelastic Tailoring of Composite Wing Structures by Laminate Layup Optimization
Author:
Affiliation:
1. Cranfield University, Cranfield, Bedford, MK43 0AL England, United Kingdom
2. Beijing University of Aeronautics and Astronautics, Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.20166
Reference17 articles.
1. Aeroelastic divergence of swept-forward composite wings including warping restraint effect
2. General formulation for the aeroelastic divergence of composite swept-forward wing structures
3. Analytical studies on static aeroelastic behavior of forward-swept composite wing structures
4. Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing
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