Hostname: page-component-586b7cd67f-t8hqh Total loading time: 0 Render date: 2024-11-23T22:52:48.911Z Has data issue: false hasContentIssue false
  • English
  • Français

Some laminated plate optimum design studies using an interactive computer programme

Published online by Cambridge University Press:  04 July 2016

J. P. H. Webber
J. P. H. Webber*
Affiliation:
Department of Aerospace Engineering, University of Bristol
Get access Rights & Permissions [Opens in a new window]

Summary

An interactive computer programme, based on linear-elastic laminated plate theory, is used to study the effect of lay-up geometry on first ply failure loads. A maximum allowable strain failure criterion is used and a number of design problems are considered where searches are made for optimum lay-up configurations for typical carbon fibre reinforced plastic properties. The relative weakness of this material in tension across the fibres, is found to have a significant effect on first ply failure loads. An optimisation technique based on principal load directions is introduced and compared with the familiar 0/90/±45 lay-up configuration.

Type
Research Article
Information
The Aeronautical Journal , Volume 92 , Issue 913 , March 1988 , pp. 107 - 114
Copyright
Copyright © Royal Aeronautical Society 1988 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Ditcher, A. K. and Webber, J. P. H. Nonlinear mechanical and thermal responses of a unidirectional carbon-fibre-reinforced plastic. J Strain Anal 1979, 14, 149–156.Google Scholar
2. Ditcher, A. K., Rhodes, F. E. and Webber, J. P. H. Non linear stress-strain behaviour of carbon fibre reinforced plastic laminates. J Strain Anal, 1981, 16, 43–51.Google Scholar
3. Jones, R. M. Mechanics of Composite Materials. McGraw-Hill, 1975.Google Scholar
4. Webber, J. P. H. SSFALP - An interactive computer programme for the stress-strain failure analysis of laminated plates. Department of Aerospace Engineering, University of Bristol, 1986.Google Scholar
5. Baldwin, J. F. Support Logic Programming, Int J Intelligent Systems. 1986, 1, (2), 73–104.Google Scholar
6. Park, W. J. An optimal design of simple symmetric laminates under the first ply failure criterion. J Compos Mater, 1982, 16, 341–355.Google Scholar