Structural design and optimization of a morphing wing trailing edge flap

Author:

Ding Shuai,Zhou XiangORCID

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Reference22 articles.

1. Li G (2017) Design and optimization of camber continuously morphing wing mechanism with multiple joints. PhD thesis, Harbin Institute of Technology

2. Huang J, Ge W (2010) Advanced and key techniques in the adaptive wing. Aero Weapon 2010(2):8–12

3. Di Matteo N, Guo S, Ahmed S, Li D (2010) Design and analysis of a morphing flap structure for high lift wing. In: 51st AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference 2010, Orlando, Florida, pp 12–21

4. Ricci S, Scotti A, Terraneo M (2006) Design, manufacturing and preliminary test results of an adaptive wing camber model. In: 48th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and material conference 2006, Newport, Rhode Island, pp 1–12

5. Voracek D, Pendleton E, Reichenbach E, Griffin K, Welch L (2003) The active aeroelastic wing phase I flight research through January 2003. In: NASA/TM 2003, NASA, Edwards, California, pp 14–22

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