...
首页> 外文期刊>Journal of Engineering Mechanics >Combination Resonance Instability of Curved Panels with Cutout Subjected to Nonuniform Loading with Damping
【24h】

Combination Resonance Instability of Curved Panels with Cutout Subjected to Nonuniform Loading with Damping

机译:阻尼不均匀载荷作用下带切口的曲面板的组合共振不稳定性

获取原文
获取原文并翻译 | 示例

摘要

The dynamic instability of doubly curved panels with a centrally located circular cutout, subjected to nonuniform compressive in-plane harmonic edge loading is investigated. The present work deals with the problem of the occurrence of combination resonances in contrast to single (mode) resonances in parametrically excited doubly curved panels with a central circular cutout. The method of multiple scales is used to obtain analytical expressions for the single (mode) and combination resonance instability regions. It is shown that other cases of the combination resonance can be of major importance and yield a significantly enlarged instability region in comparison to the principal instability region. The effects of nonuniform edge loading, centrally located circular cutout, damping, the static, and dynamic load factors on dynamic instability behavior of simply supported doubly curved panels are studied. The results show that under localized edge loading, combination resonance zones are as important as single (mode) resonance zones. The effects of damping show that there is a finite critical value of the dynamic load factor for each instability region below which doubly curved panels cannot become dynamically unstable. A central circular cutout has the destabilizing effect on the dynamic stability behavior of doubly curved panels subjected to nonuniform edge loading. This example of simultaneous excitation of two modes, each oscillating steadily at its own natural frequency, may be of considerable interest in vibration testing of actual structures.
机译:研究了中心位置为圆形切口的双曲面板在不均匀压缩面内谐波边缘载荷作用下的动态不稳定性。与具有中心圆形切口的参量激发的双弯曲面板中的单(模式)共振相反,本工作解决了组合共振的发生问题。多尺度方法用于获得单(模式)和组合共振不稳定性区域的解析表达式。已经表明,组合共振的其他情况可能是最重要的,并且与主要不稳定性区域相比,产生了显着扩大的不稳定性区域。研究了非均匀边缘载荷,位于中心的圆形切口,阻尼,静态和动态载荷因子对简单支撑的双曲面板动力不稳定性行为的影响。结果表明,在局部边缘载荷下,组合共振区与单(模)共振区同样重要。阻尼的影响表明,对于每个不稳定区域,都有一个有限的动态载荷因数临界值,在该临界值以下,双曲面板就不会变得动态不稳定。中央圆形切口对承受不均匀边缘载荷的双曲面板的动态稳定性能有破坏作用。在实际结构的振动测试中,两个模式同时激发的示例可能会引起人们极大的兴趣,这两个模式各自以其固有频率稳定振荡。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号