Study on Free Vibration Analysis of a Rotating Fibre-Graphene-Reinforced Hybrid Polymer Composites Pre-Twist Shel

Q2 Engineering
I. RAMU, Battina N. MALLESWARARAO, J. CHANDRA SEKHAR, M. VENU, P. SENTHIL KUMAR
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引用次数: 0

Abstract

The present work aims to develop a computational procedure for investigating the vibration behaviour of pre-twisted laminated composite shell containing graphene inclusions in their matrix. According to nanoscopic empirical equations, graphene's mechanical properties are determined by its size dependence. It has been demonstrated that the orthotropic mechanical properties of composite laminates made from carbon fibres and hybrid matrix can be evaluated. Based on pre-twist and geometric configurations, finite element methods have been used to model hybrid materials shells that include carbon fibre, graphene, and graphene-fibre reinforcement. As part of the validation process, the proposed method is compared with other methods when possible. Finally, the vibrational behaviour of the composite shell is extracted by imposing a twisted angle on a cantilever boundary condition. An analysis of vibrations for each configuration is presented in this paper, as well as the effects of graphene inclusions on natural frequencies. As graphene volume fractions in the matrix increase, the natural frequencies of every mode also increase. When the hub radius and rotational speed are increased, the frequency parameter increases with an increase in graphene volume in the hybrid polymer composite pre-twisted shell.
旋转纤维-石墨烯增强混杂聚合物复合材料预扭壳自由振动分析研究
目前的工作旨在开发一种计算程序来研究在其基体中含有石墨烯内含物的预扭曲层压复合材料外壳的振动行为。根据纳米尺度的经验方程,石墨烯的力学性能取决于其尺寸依赖性。结果表明,碳纤维复合材料层合板的正交各向异性力学性能是可以评价的。基于预扭和几何构型,有限元方法已被用于模拟混合材料外壳,包括碳纤维、石墨烯和石墨烯纤维增强材料。作为验证过程的一部分,在可能的情况下,将所提出的方法与其他方法进行比较。最后,通过在悬臂边界条件上施加一个转角来提取复合材料壳的振动特性。本文给出了每种结构的振动分析,以及石墨烯内含物对固有频率的影响。随着石墨烯在基体中的体积分数增加,每种模式的固有频率也增加。当轮毂半径和转速增加时,频率参数随杂化聚合物复合材料预扭壳中石墨烯体积的增加而增加。
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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