 | | Mechanics of Solids
A Journal of Russian Academy of Sciences | | Founded
in January 1966
Issued 6 times a year
Print ISSN 0025-6544
Online ISSN 1934-7936 |
Archive of Issues
| Total articles in the database: | | 12977 |
| In Russian (Èçâ. ÐÀÍ. ÌÒÒ): | | 8096
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| In English (Mech. Solids): | | 4881 |
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| Li Bowen, Zhang Jiamu, Chu Guangyuan, Zhang Feng, and Jin Peng, "Aeroelastic Analysis and Lay-Up Optimization Strategy for Glass/Carbon Fiber Hybrid Composite Panels Subjected to Supersonic Airflow," Mech. Solids. 59 (5), 3139-3147 (2024) |
| Year |
2024 |
Volume |
59 |
Number |
5 |
Pages |
3139-3147 |
| DOI |
10.1134/S0025654424605160 |
| Title |
Aeroelastic Analysis and Lay-Up Optimization Strategy for Glass/Carbon Fiber Hybrid Composite Panels Subjected to Supersonic Airflow |
| Author(s) |
Li Bowen (School of Aerospace Engineering, Huazhong University of Science and Technology, Wuan, 430070 China)
Zhang Jiamu (BeiJing Institute of Structure and Environment Engineering, Beijing, 100076 China)
Chu Guangyuan (China Academy of Launch Vehicle Technology, Beijing, 100076 China)
Zhang Feng (School of Aerospace Engineering, Huazhong University of Science and Technology, Wuan, 430070 China)
Jin Peng (School of Aerospace Engineering, Huazhong University of Science and Technology, Wuan, 430070 China, nwpu-jinpeng@163.com) |
| Abstract |
This research aimed to address the growing demand for multifunctional composite panels
with high aeroelastic stability in the aerospace industry by proposing a glass/carbon fiber hybrid composite structure suitable for aircraft wing panels and outlining an optimization strategy. The results
revealed that while increasing the hybrid ratio of glass fiber had the potential to enhance the multifunctional designability of laminated panels, it also led to decreased aeroelastic stability. However, through
the optimization of lay-ups, the negative impact of glass fiber hybridization on load-bearing performance could be mitigated, allowing for the simultaneous achievement of structural stability and multifunctional designability. |
| Keywords |
hybrid composite panels, hybrid ratio, lay-ups, aeroelastic stability, optimization |
| Received |
29 August 2024 | Revised |
06 November 2024 | Accepted |
06 November 2024 |
| Link to Fulltext |
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