ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Optimal design of adaptive compliant trailing edge based on parametric analysis
Received date: 2017-05-25
Revised date: 2017-07-18
Online published: 2017-07-18
The research introduces a kind of optimal design method of shape control for adaptive compliant trailing edge. The key design issue of the approach is the synthesis of a suitable topology for the compliant trailing edge which can produce a precise deformation. This paper illustrates the mathematic model of the topological optimization of compliant structures, and proposes a topology optimal design method based on parametric analysis for compliant trailing edge of adaptive wing. In this approach the engineering roundness and dimensional optimal procedure are followed. Finally, the optimal design method for compliant trailing edge is validated by a nonlinear finite element analysis and a functional test.
WANG Zhigang , YANG Yu , DUAN Shihui . Optimal design of adaptive compliant trailing edge based on parametric analysis[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017 , 38(S1) : 721562 -721562 . DOI: 10.7527/S1000-6893.2017.721562
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