Design and Analysis of a Morphing Flap Structure for High Lift Wing

Author:

Di Matteo Natalia,Guo Shijun,Ahmed Shakeel,Li Daochun

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. 2Kuzmina, S., Amiryants, G., Schweiger, J., Cooper, J., Amprikidis, M., and Sensberg, O. "Review and Outlook on Active and Passive Aeroelastic DesignConceptsforFuture Aircraft," ICAS Congress, 2002, pp432.1-432.10

2. 3Bae, J. S., Seigler, T. M., Inman, D. J., Lee, I. "Aerodynamic and Aeroelastic Considerations of a Variable-Span Morphing Wing", 45th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference, Palm Springs, California, 2004, pp.1-9

3. 5Ricci, S., Scotti, A., Terraneo, M. "Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model", 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, andMaterial Conference, Newport, Rhode Island, 2006, pp.1-12.

4. 6Monner, H. P., Sachau, D., and Breitbach, E. "Design Aspects of the Elastic Trailing Edge for and Adaptive Wing," RTO AVT Specialists' Meeting on Structural Aspects of Flexible Aircraft Control, Report ADP10488, Ottawa, Canada, 1999, pp14.1-14.8.

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