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A Design Framework for Thick and Thin Tow-Steered Composites Using Mechanics of Structure GenomeThe design of tow-steered composites is one of the most popular and promising topics under the class of variable stiffness structures. In this work, the authors propose a new design framework and tool for the optimization of tow-steered composites. Mechanics of structure genome (MSG) provides accurate computation of plate/shell section properties including thick and highly curved structures. The computed section properties can be directly used in commercial computer-aided engineering tools. Tow-steered composites are modeled through a design framework wherein tow paths are parameterized in a general way and projected onto a finite element mesh, and MSG calculates the local shell/plate properties. The result is a complete workflow from design parameter input to structural performance evaluation. An open-source optimization software package is used to enable constrained optimization of structural stiffness for the broad tow-steered composite design space. Numerical examples are provided to demonstrate the capabilities of this tool and the promise and potential of tow-steered designs that optimize structural performance while satisfying manufacturing constraints.
Document ID
20220018643
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Su Tian
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Yufei Long
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Xin Liu
(The University of Texas at Arlington Arlington, Texas, United States)
Frank Leone
(Langley Research Center Hampton, Virginia, United States)
Wenbin Yu
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Date Acquired
December 7, 2022
Subject Category
Composite Materials
Meeting Information
Meeting: AIAA SciTech Forum
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80NSSC21C0405
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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