Abstract
Composite materials are excellent candidates for structural optimization, as the best stacking sequence and fiber orientation varies with respect to loading condition. Typical aerospace applications experience multiple scenarios in flight, making it difficult to design a single “best” panel. While past research has explored individual cases – composite ply configuration, multiple load scenarios, and multiple performance objectives – there has been limited work addressing the interactions between these factors. This work builds upon previous efforts by constructing a Finite Element model and using multi-objective optimization techniques to explore the robustness of a composite across multiple load scenarios when considering a large number of angle orientations and competing objectives.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
