Paper Title:
Optimization Design of Composite Wing Structure of a Minitype Unmanned Aerial Vehicle
  Abstract

The application of advanced composites on the aerocraft structure can significantly reduce the weight, and improve the aerodynamic and flight performances. In this work, optimization design of a composite wing structure of a minitype unmanned aerial vehicle (UAV) is implemented. The parametric finite element model is established using parametric modeling technique for stress and stain analysis. The global optimal solution is guaranteed by the proposed two-step optimization search strategy combing genetic algorithm (GA) and sequential quadratic programming (SQP).

  Info
Periodical
Advanced Materials Research (Volumes 156-157)
Edited by
Jingtao Han, Zhengyi Jiang and Sihai Jiao
Pages
1532-1536
DOI
10.4028/www.scientific.net/AMR.156-157.1532
Citation
Y. Zhang, F. F. Xiong, S. X. Yang, X. N. Mei, "Optimization Design of Composite Wing Structure of a Minitype Unmanned Aerial Vehicle", Advanced Materials Research, Vols. 156-157, pp. 1532-1536, 2011
Online since
October 2010
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Price
$32.00
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