Optimum design of laminated fibre composite plates
β Scribed by L. A. Schmit Jr.; B. Farshi
- Publisher
- John Wiley and Sons
- Year
- 1977
- Tongue
- English
- Weight
- 982 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0029-5981
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β¦ Synopsis
Abstract
A method is presented for the minimum weight optimum design of laminated fibre composite plates, subject to multiple inplane loading conditions, which includes stiffness, strength and elastic stability constraints. The buckling analysis is based on an equivalent orthotropic plate approach leading to two uncoupled eigenproblems per load condition. Overall computational efficiency is achieved by using constraint deletion techniques in conjunction with Taylor series approximations for the constraints retained. The optimization algorithm used, namely the method of inscribed hyperspheres, is a sequence of linear programs technique which exhibits rapid convergence in this application. Several example problems are given to demonstrate that the method presented offers an efficient and practical optimum design procedure for the fundamental and recurring problem treated.
π SIMILAR VOLUMES
The vibration of skew laminated composite plates with simply supported and clamped edges is studied. The skew plate is mapped into a unit square by linear transformation. Orthogonal polynomials are used with the Ritz method to determine the natural frequencies. The e!ects of skew angle and laminatio
Two versions of a {1, 2} higher order laminate plate theory are derived for elastodynamics and used to compute natural frequencies and mode shapes for homogeneous and laminated plates. The theories include deformations due to transverse shear and transverse normal stretching and account for rotary a
## I NTRODUCTl ON Optimization techniques have now been applied to structural design for nearly thirty years. However, the great majority of this work has been limited to research activities directed at developing the methods, improving algorithms, and understanding their capabilities and limitati