Tow Path Planning Strategies for Fiber Steered Laminates
Author:
Affiliation:
1. University of South Carolina, Columbia, South Carolina 29208
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036481
Reference13 articles.
1. FayazbakhshK., The Impact of Gaps and Overlaps on Variable Stiffness Composites Manufactured by Automated Fiber Placement, McGill University, Montreal, 2013, pp. 55–83.
2. Experimental study of the effect of automated fiber placement induced defects on performance of composite laminates
3. Defect layer method to capture effect of gaps and overlaps in variable stiffness laminates made by Automated Fiber Placement
4. A Theoretical Model to Study the Influence of Tow-drop Areas on the Stiffness and Strength of Variable-stiffness Laminates
5. Optimization of course locations in fiber-placed panels for general fiber angle distributions
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1. Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering;Journal of Aircraft;2024-07
2. Tow Path Recovery and Quantification of Manufacturing Constraints for Tow Steered Composite Structures;AIAA SCITECH 2024 Forum;2024-01-04
3. Design Framework for Optimization of Curvilinearly Stiffened Variable Stiffness Composite Laminates with Direct Fiber Angle Parameterization;AIAA SCITECH 2024 Forum;2024-01-04
4. Vibration suppression of composite panel with variable angle tow design and inerter-based nonlinear energy sink;Journal of Zhejiang University-SCIENCE A;2023-08
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