Abstract
There is a great demand for optimization of high performance composite structures, particularly in the aerospace sector. To avoid vibrational resonance in aerospace and naval structures, laminated plates can be designed using fundamental frequency constraints. Composite panels are particularly attractive because the vibration response can be optimised by tailoring the fibre angles of different layers without incurring weight penalties. A viable alternative is to use circumferential and radial layers for optimizing fundamental frequencies. This work focuses on the application these two types of theoretical layers and investigating its efficiency, for plates with and without cutouts.
Original language | English |
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Title of host publication | AIAA Scitech 2021 Forum |
Subtitle of host publication | 11–15 & 19–21 January 2021Virtual/online event |
Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
Number of pages | 14 |
ISBN (Electronic) | 978-1-62410-609-5 |
DOIs | |
Publication status | Published - 2021 |
Event | AIAA Scitech 2021 Forum - Virtual/online event due to COVID-19 , Virtual, Online Duration: 11 Jan 2021 → 21 Jan 2021 |
Conference
Conference | AIAA Scitech 2021 Forum |
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City | Virtual, Online |
Period | 11/01/21 → 21/01/21 |