A single-level composite structure optimization method based on a blending tapered model-Reference-Cited by-同舟云学术

A single-level composite structure optimization method based on a blending tapered model

Published:2013-08 Issue:4 Volume:26 Page:943-947
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

An Weigang,Chen Dianyu,Jin Peng

Funder

National Natural Science Foundation of China

Foundation Sciences of Northwestern Polytechnical University

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference20 articles.

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4. Toropov VV, Jones R, Willment T. Weight and manufacturability optimization of composite aircraft components based on a genetic algorithm. In: Proceedings of Sixth World Congress of SMO; 2005.

5. Stacking sequence blending of multiple composite laminates using genetic algorithm;Soremekun;Compos Struct,2002

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