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Aerodynamic Performance of the Three-Dimensional Lumped Flexibility Bionic Hovering Wing
2018
International Journal of Aerospace Engineering
Understanding the effect of flexibility on the aerodynamic characteristics of the wing is one of the most important considerations for successfully designing a flapping wing micro aero vehicle (FMAV). This paper aims at providing a systematic synthesis on the flexibility effects on the hovering performance of the bionic wing based on the numerical analysis approach. We construct a novel three-dimensional bionic wing, which has lumped flexibility at the root, and develop an iterative coupling
doi:10.1155/2018/1314258
fatcat:cbkk7la6kbfzzdkzojnbgpgfwa