Stiffness Corrections for Overlaps and Gaps in Steered Composite Panel Optimization

Conference Paper (2017)
Author(s)

Michel van Tooren (University of South Carolina)

Ali Elham (TU Delft - Flight Performance and Propulsion)

D.A. Lucas (University of South Carolina)

Research Group
Flight Performance and Propulsion
DOI related publication
https://doi.org/10.2514/6.2017-0895
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Publication Year
2017
Language
English
Research Group
Flight Performance and Propulsion
Article number
AIAA 2017-0895
ISBN (electronic)
978-1-62410-453-4
Event
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2017-01-09 - 2017-01-13), Grapevine, United States
Downloads counter
154

Abstract

In this paper, a method is introduced that predicts the influence of gaps and overlaps introduced by fiber steering on the stiffness and strength of composite laminates. This method is based on the incorporation of a “density functional” which translates the effect of discrete gaps and laps into a continuous correction of the reduced stiffness matrix. It also includes a function to incorporate a fiber placement manufacturing strategy. Test configurations used to test the validity of the density functional approach show results consistent with the expected gap/overlap distributions, and also demonstrate the robustness of the manufacturing strategy function. The method is to be included in the TopSteer optimization code1 to study the influence of gaps and overlaps on optimization results.

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