Optimization of a Panelled Smooth Composite Shell with a Closed Cross-Sectional Contour by Using a Genetic Algorithm-Reference-Cited by-同舟云学术

Optimization of a Panelled Smooth Composite Shell with a Closed Cross-Sectional Contour by Using a Genetic Algorithm

Published:2013-10-31 Issue:5 Volume:49 Page:563-570
ISSN:0191-5665
Container-title:Mechanics of Composite Materials
language:en
Short-container-title:Mech Compos Mater

Author:

Symonov V. S.,Karpov I. S.,Juračka J.

Publisher

Springer Science and Business Media LLC

Subject

Polymers and Plastics,Mechanics of Materials,Condensed Matter Physics,General Mathematics,Biomaterials,Ceramics and Composites

Link

http://link.springer.com/content/pdf/10.1007/s11029-013-9372-0.pdf

Reference8 articles.

1. Airbus S.A.S.: [website]. URL: http://www.airbus.com (reference date: 01.03.2013).

2. The Boeing Company: [website]. URL: http://www.boeing.com (reference date: 01.03.2013).

3. V. V. Vasilev, Mechanics of Composite Structures [in Russian], Mashinostroenie, Moscow (1988).

4. I. S.Karpov, Design of Composite Parts and Units [in Russian]: Handbook, N. Y. Zhukovsky National Aerospace University “KhAI”, Kharkov (2010).

5. V. S. Symonov, “Optimization of a Panelled Smooth Composite Shell with a Single-Cell Closed Section,” [in Russian], Design and Production Issues of Flying Vehicle Structures: Collection of Scientific Papers of the N. Y. Zhukovsky National Aerospace University “KhAI”, NAKU, Kharkov, 57, No. 1, 13-23 (2009).

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