各向同性和正交异性层压板FVA的分析与实验研究及有限元验证

Q2 Engineering
K. Srividya, P. Anusha, E. Kavitha, M. Naga Swapna Sri, V. Sravani
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引用次数: 0

摘要

二维剪切变形和高阶理论、三维精确弹性法和二维、三维有限元法等方法可用于预测复合材料层合板的固有频率。总之,三维有限元法有助于开发具有复杂约束、材料和复杂几何形状的结构模型。但有限元指导了一种方法,该方法根据离散化类型和场变量限制所需的多项式方法获得解的近似值。因此,为了提高有限元结果的准确性,并与其他基准结果进行验证,在有限元的基础上进行了收敛性测试。本文采用三维有限元方法对各向同性和正交异性材料的矩形厚板自由振动分析的几种边界条件进行了求解,并将收敛结果与已有的解析结果进行了比较。此外,还对厚各向同性和正交各向异性材料进行了试验,并进行了试验模态分析,以验证三维有限元过程。从本研究可知,有限元方法的数值与各向同性材料的各种实验和分析结果高度收敛。将三维有限元分析结果与正交各向异性试样的实验结果进行比较,偏差为5-8%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Analytical and Experimental study on FVA of Isotropic and Orthotropic Laminates with FEM Validations
Several approaches such as two-dimensional shear deformation and higher order theories, three-dimensional exact elasticity method and 2-D, 3-D finite element procedures are available in predicting the natural frequencies of composite laminates. In all, a 3-D FEM assists in developing a model for structures with complex constraints, materials and complex geometries. But FE directs an approach that obtains an approximation in solution that depends on discretization type and the polynomials method desirable for field variable limitations. Hence, a convergence test is performed in addition to FE in order to improvise the finite element results accuracy and validating with other benchmark outcomes. The current investigation involves the solving for several boundary conditions of a thick rectangular plate’s free vibration analysis [FVA] for isotropic and orthotropic materials by the application of 3-D finite element methods and convergence results are compared with available analytical results. In addition, experiments are conducted on thick isotropic and orthotropic materials along with experimental modal analysis in order to verify 3-Dimensional finite element process. From this study it can be known that, the values of finite element method highly converges with various experimental and analytical results of isotropic material. When comparing 3-D FEM with the experimental results of the orthotropic sample, a deviation of 5-8% was observed.
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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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