热-热-机械复合载荷下弹性地基中dwbnnt加固压电柱壳扭转屈曲非线性响应

M. Sarvandi, M. Najafizadeh, H. Seyyedhasani
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引用次数: 2

摘要

纳米复合材料提供了新的性能,并利用了材料之间独特的协同作用。聚偏氟乙烯(PVDF)是一种理想的压电基体,广泛应用于石油、天然气、电子和汽车等行业的纳米复合材料中。氮化硼纳米管(BNNTs)具有较高的力学、电学和化学性能。本文研究了双壁bnnt增强PVDF复合管在电-热-机械复合载荷作用下的临界扭转载荷。首先,将纳米复合材料智能管建模为弹性地基中的各向同性圆柱壳。其次,利用经典壳理论,推导了应变-位移方程,得到了荷载和弯矩。然后,确定总能量方程,由壳的应变能、外部功的能量和弹性基础的能量组成。此外,利用欧拉方程,在圆柱坐标系中导出了三正交的平衡方程;然后,通过相邻点的等效方法建立了稳定性方程。利用波动法求解所建立的方程以获得临界扭转力矩。结果表明:所研究的圆柱壳在轴向半波数m = 24,周向半波数n = 1时发生临界扭转屈曲载荷;结果还表明,临界扭转屈曲载荷随长半径比和半径壳厚比的增大而增大和减小。最后,通过数值方法对不同状态下的结果进行了比较。此外,通过与文献中壳层方程和板层方程的比较,验证了稳定性方程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Non-Linear Response of Torsional Buckling Piezoelectric Cylindrical Shell Reinforced with DWBNNTs Under Combination of Electro-Thermo-Mechanical Loadings in Elastic Foundation
Nanocomposites provide new properties and exploit unique synergism between materials. Polyvinylidene fluoride (PVDF) is an ideal piezoelectric matrix applicable in nanocomposites in a broad range of industries from oil and gas to electronics and automotive. And boron nitride nanotubes (BNNTs) show high mechanical, electrical and chemical properties. In this paper, the critical torsional load of a composite tube made of PVDF reinforced with double-walled BNNTs is investigated, under a combination of electro-thermo-mechanical loading. First, a nanocomposite smart tube is modeled as an isotropic cylindrical shell in an elastic foundation. Next, employing the classical shell theory, strain-displacement equations are derived so loads and moments are obtained. Then, the total energy equation is determined, consisting of strain energy of shell, energy due to external work, and energy due to elastic foundation. Additionally, equilibrium equations are derived in cylindrical coordinates as triply orthogonal, utilizing Euler equations; subsequently, stability equations are developed through the equivalent method in adjacent points. The developed equations are solved using the wave technique to achieve critical torsional torque. Results indicated that critical torsional buckling load occurred in axial half-wave number m = 24 and circumferential wave number n = 1, for the investigated cylindrical shell. The results also showed that with the increase in the length-to-radius ratio and in the radius-to-shell thickness ratio, the critical torsional buckling load increased and decreased, respectively. Lastly, results are compared in various states through a numerical method. Moreover, stability equations are validated via comparison with the shell and sheet equations in the literature.
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