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A laser velocity gradient and vorticity probe for turbulent shear flows.

机译:用于湍流剪切流的激光速度梯度和涡度探头。

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A laser-based probe for the direct, non-intrusive measurement of temporally- and spatially-resolved velocity gradient and vorticity was developed and demonstrated. The optical probes developed were used in turbulent two-stream mixing layers as well as laminar and turbulent boundary layers for the measurement of several velocity gradients and spanwise vorticity. The measurement technique is based on the collection and direct heterodyning of coherent light scattered from particles in two adjacent locations allowing the determination of a velocity gradient. The beat frequency of the heterodyned light gives the difference in the Doppler shift and is proportional to the velocity difference of two points. This frequency is analyzed using a conventional laser Doppler velocimetry (LDV) signal processor (in the present, a burst spectrum analyzer). The angle between the laser beam and the direction of the scattered light determines the measured component of velocity. Therefore, a component of the vorticity vector is measured by using two sets of transmitting and collecting optics, focused at a single location, along with two LDV processors. The technique is non-intrusive, straightforward and relatively inexpensive since it uses standard, off-the-shelf optical and electronic components. It also allows the development of a compact probe with integrated instrumentation. In the present research, the time-frozen measurements of ∂u/∂ y, ∂v/∂x, ∂ v/∂y in the boundary and mixing layers were carried out using the laser velocity gradient (LVG) probe. Time-frozen measurements of the spanwise component of vorticity were also carried out using the laser vorticity probe (LVP) which is composed of, essentially, two sets of LVG probes. LVG and LVP measurements are compared to LDV measurements and data available in the literature. These measurements demonstrated the viability of the new measurement technique as a research tool. Analyses and several systematic measurements were also performed to determine the data rates and the intrinsic measurement uncertainty associated with the technique.
机译:基于激光的探头可以直接,非侵入性地测量时间和空间分辨的速度梯度和涡度。开发的光学探头用于湍流两流混合层以及层流和湍流边界层中,用于测量几个速度梯度和翼展方向涡度。测量技术基于从两个相邻位置的粒子散射的相干光的收集和直接外差作用,从而可以确定速度梯度。杂散光的拍频给出了多普勒频移的差异,并且与两点的速度差异成正比。使用常规的激光多普勒测速(LDV)信号处理器(当前为脉冲频谱分析仪)分析该频率。激光束与散射光方向之间的夹角决定了测得的速度分量。因此,通过使用聚焦在单个位置的两组发射和采集光学器件以及两个LDV处理器来测量涡度矢量的分量。由于该技术使用标准的现成光学和电子组件,因此它是非侵入性的,直接的且相对便宜的。它还允许开发带有集成仪器的紧凑型探头。在本研究中,使用激光速度梯度(LVG)探针对边界层和混合层中的∂u/∂y,∂v/∂x,∂v/∂y进行了时间冻结测量。还使用激光涡旋探头(LVP)对涡旋的跨度分量进行了时间冻结测量,该探头实际上由两组LVG探头组成。将LVG和LVP测量与LDV测量和文献中提供的数据进行比较。这些测量结果证明了新的测量技术作为研究工具的可行性。还进行了分析和一些系统的测量,以确定与该技术相关的数据速率和固有测量不确定性。

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