A new framework for optimization of variable stiffness plates

Conference Paper (2017)
Author(s)

D. Barazanchy (University of South Carolina)

MJL van Tooren (University of South Carolina)

BF Tatting (University of South Carolina)

A Elham (TU Delft - Flight Performance and Propulsion)

Research Group
Flight Performance and Propulsion
DOI related publication
https://doi.org/10.2514/6.2017-0894
More Info
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Publication Year
2017
Language
English
Research Group
Flight Performance and Propulsion
ISBN (electronic)
978-1-62410-453-4

Abstract

An alternative to the lamination parameters framework is proposed that uses the fiber angles as design variables: the manufacturing finite element mesh (MFEM) framework. The structure and implementation of the MFEM framework allows for both stiffness and strength constraints. In this manuscript the maximum failure index is minimized the case of a static analysis, while for buckling analysis the first buckling mode is maximized. For each case example are presented and discussed. To complete the manuscript the post- processing tool used to obtain feasible automated fiber placement machine tow paths is briey discussed.

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