Snap-Through Buckling

R. Wiebe, L. Virgin, I. Stanciulescu, S. Spottswood
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引用次数: 9

Abstract

Snap-through buckling can reduce the life-span of structural systems such as aircraft surface paneling. This is envisioned to be a specific problem in hypersonic vehicles in which severe thermal loading and acoustic excitation conspire to create an especially hostile environment for structural elements. A shallow arch, and two simplified link models are used to investigate the mechanisms of snap-through buckling from a fundamental, or phenomenological, standpoint. The complexities introduced by modal interactions are introduced and a method for identifying snap-through buckling is developed.
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入屈曲
通过卡扣屈曲可以减少结构系统的寿命,如飞机表面镶板。这被设想为高超音速飞行器中的一个特定问题,在这种飞行器中,严重的热载荷和声激励共同创造了一个对结构元件特别不利的环境。一个浅拱和两个简化的链接模型被用来从基本的或现象学的角度来研究通过屈曲的机制。介绍了模态相互作用带来的复杂性,并提出了一种识别卡断屈曲的方法。
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