首页> 外文会议>NCA-vol.32; American Society of Mechanical Engineers(ASME) International Mechanical Engineering Congress and Exposition; 20051105-11; Orlando,FL(US) >CHALLENGES OF INVESTIGATING FLUID-ELASTIC LOCK-IN OF A SHALLOW CAVITY AND A CANTILEVERED BEAM AT LOW MACH NUMBERS
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CHALLENGES OF INVESTIGATING FLUID-ELASTIC LOCK-IN OF A SHALLOW CAVITY AND A CANTILEVERED BEAM AT LOW MACH NUMBERS

机译:低模数下浅腔和悬臂梁的流体弹性锁定研究的挑战

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At low flow Mach numbers, fluid-elastic lock-in may occur when a shear layer instability interacts with an adjoining or nearby structure and the resulting vibration of the structure reinforces the shear layer instability. Despite the significant amount of study of lock-in with acoustic resonators, fluid-elastic lock-in of a shear layer fluctuation over a cavity and a structural resonator is not well understood and has not been thoroughly studied. Design of an experimental system is described and preliminary diagnostics are addressed as a basis for a platform for developing a fundamental understanding of the feedback mechanism, analytical models for predicting and describing fluid-elastic lock-in conditions, and the roles of the fluid and structural dynamics in the process. Features of the system investigated here include design for characterization of modal excitation of a beam-like structure from the shear layer fluctuation, isolation of the predominant instability source to the shear layer fluctuation over the cavity, variation of the cavity size to identify critical parameters that govern fluid-elastic lock-in, and alteration of the inflow boundary layer momentum thickness. So far, lock-in between the cavity and the distributed elastic resonator has not been achieved. Further investigations to determine the role of the source and resonator attributes are underway.
机译:在低马赫数下,当剪切层的不稳定性与相邻或附近的结构相互作用时,可能会发生流体弹性锁定,并且结构的最终振动会增强剪切层的不稳定性。尽管对声谐振器的锁定进行了大量的研究,但对空腔和结构谐振器上的剪切层起伏的流体弹性锁定仍然知之甚少,并且尚未进行深入研究。描述了实验系统的设计,并提出了初步的诊断方法,以此为基础建立了对反馈机制的基本了解,用于预测和描述流体弹性锁定条件的分析模型以及流体和结构的作用的平台过程中的动态。此处研究的系统的特征包括:从剪切层起伏表征梁状结构的模态激励的设计,将主要不稳定性源隔离到模腔上的剪切层起伏,模腔尺寸变化以识别关键参数的设计。控制流体弹性锁定,并改变流入边界层的动量厚度。到目前为止,还没有实现空腔与分布式弹性谐振器之间的锁定。确定源和谐振器属性作用的进一步研究正在进行中。

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