Optimal Design of Tow-Steered Composite Laminates with Curvilinear Stiffeners
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2243
Reference19 articles.
1. Optimum stacking sequence design of composite materials Part II: Variable stiffness design
2. Surrogate-based multi-objective optimization of a composite laminate with curvilinear fibers
3. Design of variable-stiffness composite panels for maximum buckling load
4. Optimization of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring
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1. Design Framework for Optimization of Curvilinearly Stiffened Variable Stiffness Composite Laminates with Direct Fiber Angle Parameterization;AIAA SCITECH 2024 Forum;2024-01-04
2. An Integrated Design Tool for Tow-steering Composites in Abaqus and MSC.Patran/Nastran;AIAA SCITECH 2023 Forum;2023-01-19
3. Fast analysis of curvilinearly stiffened panels operating in the postbuckling field;Mechanics of Advanced Materials and Structures;2022-11-15
4. Buckling performance of curvilinearly grid-stiffened tow-placed composite panels considering manufacturing constraints;Composite Structures;2021-03
5. Pre-buckling and Buckling Analysis of Variable-Stiffness, Curvilinearly Stiffened Panels;Aerotecnica Missili & Spazio;2019-12-10
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