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Vibration and Buckling Analysis of Multifunctional Antenna Structures with Thermoelastic Characteristics : 열 효과를 고려한 다기능 내장 안테나 구조물의 진동과 좌굴 해석

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Authors

Kang Seok Hyeon

Advisor
김지환
Major
공과대학 기계항공공학부
Issue Date
2017-02
Publisher
서울대학교 대학원
Keywords
Multifunctional antenna structureBucklingVibrationFlutterHeat conduction.
Description
학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2017. 2. 김지환.
Abstract
The performance of multifunctional antenna structure contained inside of the aircraft structure is analyzed under the influence of vibration caused by airflow and a thermal environment. The model is a multi-layer sandwich structure composed of carbon/epoxy, glass/epoxy and a dielectric polymer which is assumed to be an antenna. The First-order Shear Deformation Theory (FSDT) is used with a modified shear correction factor. In order to account for a geometrical nonlinearity, the governing equations are based on the von-Karman displacement-strain relationship with the principle of virtual work. Additionally, using the first-order piston theory, the effect of aerodynamic pressure is represented in the equation. The Newton-Rhapson iteration and the Newmark method is used to solve the nonlinear equation and the time analysis, respectively. Also, neutral surface and shear correction factor concepts are studied for unsymmetric models. The thermal environment is generally considered with one-dimensional heat conduction equations. To check the validity of the results, it is compared to the numerical data of vibration and buckling from previous studies. Post-buckling and flutter analysis is performed with simply-supported and clamped boundary conditions.
Language
English
URI
https://hdl.handle.net/10371/123961
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