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Effect of Loading on the Snap-through Response of a Post-buckled Beam

机译:负载对后弯梁梁的快照响应的影响

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Snap-through response is a post-buckling phenomenon, which results in large amplitude motion between the equilibrium configurations. This paper provides some observations on snap-through response of a flat-beam specimen through both experiments and simulations based on experimentally motivated parameter values. The effect of static (thermal) loading and dynamic loading is investigated for its effect on snap-through response. It is shown that snap-through response frequency increases with increasing dynamic load but decreases with increasing static load. Further, snap-through response amplitude increases both with increasing dynamic load and with increasing static load. This research analyzes the characteristic of snap-through response frequency and suggests that the paradigm of intermittent and persistent snap-through should shift to a snap-through response frequency spectrum. A reduced-order modal model of the flat beam is used to numerically estimate a snap-through boundary in the parameter space of loading. These results contribute to the development of an analytic snap-through boundary. Although a conservative estimate for this boundary can be obtained via energy principles, this research seeks to establish a detailed characterization of snap-through response such that it could lead to design criteria for non-conservative aerospace structures. A sensitivity analysis is then conducted on the snap-through boundary. This analysis includes variations in linear stiffness, nonlinear stiffness and damping.
机译:快照响应是后屈曲现象,从而导致平衡配置之间的大幅度运动。本文通过基于实验动机参数值的实验和模拟,提供了一些关于扁平梁样本的响应的一些观察结果。研究了静态(热)载荷和动态载荷的影响,以实现对快速响应的影响。结果表明,随着动态负载的增加而增加,卡通响应频率随而随着静态负载的增加而降低。此外,随着动态负载的增加和静态负载增加,卡通响应幅度都会增加。该研究分析了快速响应频率的特性,并表明间歇和持久快速的范例应该转移到快速响应频谱频谱。平光束的减小阶模型模型用于数值估计加载参数空间中的快速边界。这些结果有助于开发分析捕获边界。尽管可以通过能量原理获得该边界的保守估计,但是该研究旨在建立快速响应的详细表征,使得它可能导致非保守航空航天结构的设计标准。然后在快速边界上进行灵敏度分析。该分析包括线性刚度,非线性刚度和阻尼的变化。

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