Affiliation:
1. University of Liverpool
Publisher
American Institute of Aeronautics and Astronautics
Reference44 articles.
1. Aeroelastic Tailoring of Forward Swept Composite Wings
2. Application of Genetic Algorithm for Aeroelastic Tailoring of a Cranked-Arrow Wing
3. 5M. Kameyama, H. Fukunaga., Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters. Computers and structures85(2007),pp.213-224.
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3 articles.
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