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Design for Manufacturing Tool for Automated Fiber Placement Structures - Verification and Validation A tool has been developed to address the growing Design for Manufacturing needs for composite structures, specifically those manufactured with automated fiber placement. This manufacturing approach presents unique challenges associated with puckers and wrinkling, tow overlaps and gaps, fiber deviation, and laminate strength. Achieving a satisfactory laminate design usually requires finding compromises between those four areas. The developed tool, dubbed the Central Optimizer, assists with the process of balancing competing design metrics in automated fiber placement. This tool was developed under the NASA Advanced Composites Consortium with input from industry partners. Under this program, the Central Optimizer has been exercised on three different structures to verify its functionality and validate ability to improve the design process for automated fiber placement structures.
Document ID
20200002929
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
August T Noevere
(Collier Research Corporation Newport News, Virginia, United States)
Craig S Collier
(Collier Research Corporation Newport News, Virginia, United States)
Date Acquired
April 22, 2020
Publication Date
January 6, 2020
Publication Information
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Computer Programming And Software
Report/Patent Number
NF1676L-33454
AIAA 2020-1477
Report Number: NF1676L-33454
Meeting Information
Meeting: AIAA SciTech Exhibition and Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2020
End Date: January 10, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 826611.04.07.03
CONTRACT_GRANT: NNL09AA00A
CONTRACT_GRANT: 80LARC17C0004
Distribution Limits
Public
Copyright
Public Use Permitted.
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