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Self-excited oscillations of flow past deep cavities: Effect of variable damping.

机译:流经深腔的自激振荡:可变阻尼的影响。

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摘要

The overall objective of this investigation is to determine the effect of variable damping on the pressure response characteristics of a deep cavity. The pressure fluctuations arise from coupling between the unsteady shear layer along the cavity opening and a resonant acoustic mode of the cavity. Damping of the cavity is represented by the quality (Q) factor, which is determined from external acoustic excitation in the absence of mean flow. The value of the Q factor can be varied continuously with a damping device, which is located at the dead end of the cavity; it allows variation of the magnitude of damping without changes of the geometry or parameters of the deep cavity.;The amplitude of the pressure fluctuation as a function of flow velocity is characterized for the first, second and third depth-wise acoustic modes, which are generated in cavities with different depths. For each mode, the value of the Q factor is varied over a relatively wide range. Substantial attenuation of the pressure amplitude is attained. For higher acoustic modes, and at sufficiently high values of cavity damping, corresponding to low values of Q factor, abrupt decreases or drop-offs of the pressure amplitude occur at threshold values of flow velocity. Moreover, the peak response amplitude occurs at values of dimensionless frequency (Strouhal number) that increase with decreasing values of the Q factor.;The amplitude of the unsteady pressure oscillations (normalized by the freestream dynamic head) generally exhibits a linear variation with Q factor, for four depth-wise acoustic modes of the cavity. Furthermore, the strength of lock-on (SoL) of the pressure oscillation, as a function of Q factor, is evaluated in terms of the coherent and broadband (background) pressure amplitudes. Not only the coherent pressure amplitude, but also the broadband amplitude, is attenuated for decreasing values of Q factor. As a consequence, variation of the strength of lock-on with Q factor must account for both of these effects.;Quantitative imaging, in the form of high-image-density particle image velocimetry (PIV), is employed to characterize the flow structure of coupled oscillations arising from the shear layer along the opening of the deep cavity. Time- and phase-averaged patterns provide insight into the effect of resonator damping on the flow structure. In essence, when the Q factor of the cavity decreases, attenuation of the pressure amplitude at the dead end of the cavity is accompanied by corresponding attenuation of the shear layer undulation along the cavity opening. Cross-comparison of patterns of velocity vectors, streamwise and transverse velocity components, as well as vorticity, illustrate the detailed features of the damped oscillations of the shear layer.;Quantitative imaging also provides a basis for determination of the hydrodynamic contributions to the acoustic power, as well as calculation of the total acoustic power, which is generated by the oscillating shear layer in presence of the resonant acoustic field of the cavity. The manner in which this power is altered in relation to the damping of the cavity is assessed, and patterns of the spatial distribution of acoustic power are related to corresponding patterns of vorticity, as well as to patterns of streamwise and transverse components of the hydrodynamic contribution to the acoustic power integral.;Prediction of the pressure oscillation amplitudes within the resonator, and the frequencies at which these oscillations occur, were undertaken using a published theoretical model, which was adapted for the deep cavity system of interest herein. Comparison of predictions with experiments shows generally good agreement, and verifies the Q factor as a representation of cavity damping, even in presence of flow.
机译:这项研究的总体目标是确定可变阻尼对深腔压力响应特性的影响。压力波动是由沿着腔体开口的非恒定剪切层与腔体的共振声模之间的耦合引起的。腔的阻尼由质量(Q)因子表示,该因子由在没有平均流量的情况下的外部声激发确定。 Q系数的值可以通过位于空腔死角的阻尼装置连续变化。它可以改变阻尼的大小而无需改变深腔的几何形状或参数。在第一,第二和第三深度声模中,压力波动幅度是流速的函数。在具有不同深度的型腔中产生。对于每种模式,Q因子的值都在相对较大的范围内变化。压力幅度得到了很大的衰减。对于较高的声学模式,并且在足够高的腔体阻尼值(对应于Q因子的低值)下,在流速阈值处会出现压力幅度的突然减小或下降。此外,峰值响应幅度出现在无因次频率(斯特劳哈尔数)的值上,该值随Q因子值的减小而增加。;非稳态压力振荡的幅度(由自由流动力头标准化)通常随Q因子呈现线性变化,用于腔体的四个深度方向声模。此外,根据相干和宽带(背景)压力幅度评估压力振荡的锁定强度(SoL)作为Q因子的函数。对于Q值的减小,不仅相干压力幅度而且宽带幅度都被衰减。因此,锁定强度随Q因子的变化必须考虑到这两种影响。;采用高图像密度颗粒图像测速(PIV)形式的定量成像来表征流动结构沿深腔开口处的剪切层产生的耦合振荡的变化。时间和相位平均模式可以深入了解谐振器阻尼对流动结构的影响。本质上,当空腔的Q因子减小时,空腔死角处压力幅度的衰减将伴随着沿着空腔开口的剪切层波动的相应衰减。速度矢量,流向和横向速度分量以及涡度的模式的交叉比较说明了剪切层阻尼振荡的详细特征。定量成像还为确定流体动力对声功率的贡献提供了基础以及计算总声功率,该总声功率是在空腔的共振声场存在时由振荡剪切层产生的。评估了相对于腔体阻尼改变此功率的方式,并且声功率的空间分布模式与相应的涡度模式以及流体动力贡献的沿流和横向分量的模式有关使用公开的理论模型对谐振器内的压力振荡幅度以及发生这些振荡的频率进行了预测,该理论模型适用于本文所关注的深腔系统。将预测结果与实验结果进行比较,通常可以得出很好的一致性,并且即使在存在流动的情况下,也可以验证Q因子是否可以表示腔体阻尼。

著录项

  • 作者

    Tinar, Egemen.;

  • 作者单位

    Lehigh University.;

  • 授予单位 Lehigh University.;
  • 学科 Engineering Aerospace.;Engineering Mechanical.;Physics Acoustics.
  • 学位 Ph.D.
  • 年度 2012
  • 页码 269 p.
  • 总页数 269
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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