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Minimum weight design of composite hybrid shells via symbolic computation

✍ Scribed by M. Walker; T. Reiss; S. Adali


Publisher
Elsevier Science
Year
1997
Tongue
English
Weight
619 KB
Volume
334
Category
Article
ISSN
0016-0032

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✦ Synopsis


The best layup for a hybrid laminated cylindrical shell subject to a buckling load constraint is determined. The objective of the optimisation is the minimum weight design of these structures. The ply angle is taken as the design variable. Various contgurations of graphite and boron epoxy layers are considered in order to determine an optimal stacking sequence. The symbolic computational software package MATHEMATICA is used in the implementation and solution of the problem. This approach simplifies the computational procedure as well as the implementation of the analysisloptimisation routine. Results are given illustrating the dependence of the optimal layup on the cylinder length and radius. It is shown that a general purpose computer algebra system like MATHEMATICA

is well suited to solve structural design problems involving composite materials.