A technique for optimally designing fibre-reinforced laminated plates under in-plane loads for minimum weight with manufacturing uncertainties accounted for-Reference-Cited by-同舟云学术

A technique for optimally designing fibre-reinforced laminated plates under in-plane loads for minimum weight with manufacturing uncertainties accounted for

Published:2006-05-30 Issue:4 Volume:21 Page:282-288
ISSN:0177-0667
Container-title:Engineering with Computers
language:en
Short-container-title:Engineering with Computers

Author:

Walker M.,Hamilton R.

Publisher

Springer Science and Business Media LLC

Subject

Computer Science Applications,General Engineering,Modeling and Simulation,Software

Link

http://link.springer.com/content/pdf/10.1007/s00366-006-0017-y.pdf

Reference27 articles.

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2. Tauchert TR, Adibhatla A (1984) Design of laminated plates for maximum stiffness. J Compos Mater 18:58–69

3. Quian B, Reiss R, Aung W (1990) The maximum stiffness design of rectangular symmetric angle-ply laminates. In: Proceedings of the 2nd international conference on computer aided design in composite material technology. Free University of Brussels/Wessex Institute of Technology, Computational Mechanics Publications, Southampton, pp 451–464

4. Kengtung C (1986) Sensitivity analysis and a mixed approach to the optimisation of symmetric layered composite plates. Eng Optim 9:233–248

5. Kam TY, Chang RR (1992) Optimum layup of thick laminated composite plates for maximum stiffness. Eng Optim 19:237–249

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