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Free flexural vibration analysis of symmetric rectangular honeycomb panels with SCSC edge supports

机译:具有SCSC边缘支撑的对称矩形蜂窝板的自由弯曲振动分析

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摘要

The free flexural vibration of symmetric rectangular honeycomb panels having SCSC edge supports is investigated in this paper using the classical plate theory and Reddy's third-order plate theory. The honeycomb core of hexagonal cells is modeled as a thick layer of orthotropic material whose physical and mechanical properties are determined using the corrected Gibson's formula. The comparative studies conducted on aluminum honeycomb panels indicate that the classical plate theories are inadequate for the flexural vibration of honeycomb panels.
机译:本文利用经典板理论和雷迪三阶板理论研究了具有SCSC边缘支撑的对称矩形蜂窝板的自由挠曲振动。六角形蜂窝的蜂窝状核心被建模为正交各向异性材料的厚层,其物理和机械性能使用校正的吉布森公式确定。在铝蜂窝板上进行的比较研究表明,经典的板理论不足以应对蜂窝板的弯曲振动。

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