Li Bowen, Zhang Jiamu, Chu Guangyuan, Zhang Feng, Jin Peng
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引用次数: 0
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.
期刊介绍：
Mechanics of Solids publishes articles in the general areas of dynamics of particles and rigid bodies and the mechanics of deformable solids. The journal has a goal of being a comprehensive record of up-to-the-minute research results. The journal coverage is vibration of discrete and continuous systems; stability and optimization of mechanical systems; automatic control theory; dynamics of multiple body systems; elasticity, viscoelasticity and plasticity; mechanics of composite materials; theory of structures and structural stability; wave propagation and impact of solids; fracture mechanics; micromechanics of solids; mechanics of granular and geological materials; structure-fluid interaction; mechanical behavior of materials; gyroscopes and navigation systems; and nanomechanics. Most of the articles in the journal are theoretical and analytical. They present a blend of basic mechanics theory with analysis of contemporary technological problems.
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