Abdallah S A, Hwang N H
Cardiovascular Flow Dynamics Laboratory, University of Houston, Texas 77004.
J Acoust Soc Am. 1988 Jan;83(1):318-34. doi: 10.1121/1.396433.
The flow field distal to an arterial stenosis is simulated by a confined turbulent jet with moderate Reynolds numbers. The wall pressure fluctuations are related to the momentum fluctuations of the jet by the Poisson equation. A Green's function was derived to satisfy the boundary conditions on a cylindrical surface. This allows the solution of the Poisson's equation to include only a volume integral of the fluctuating momentum, weighed by the relative distance between the source and the sensor. The velocity fluctuations on the jet centerline and at the middle of the shear layer were measured using a laser Doppler anemometer. The wall pressure fluctuations were detected simultaneously by an array of nine wall-mounted pressure transducers along the axial direction. Cross correlation performed between the velocity and pressure fluctuations reveals that the pressure fluctuations were mostly imposed by the passage of turbulent eddies with a convective velocity that is a function of the jet exit velocity. The Strouhal number, defined by the frequency of the passing large-scale structure, is a function of the initial conditions only very close to the jet exit. Further downstream, where the effect of the initial conditions is lost, the Strouhal number approaches a constant irrespect of the jet Reynolds number. The contribution of a source near the jet exit to wall pressure fluctuation near the reattachment is rather weak due to the rapidly decaying weighting function in the axial direction. However, for sources located within one nozzle diameter from the sensor, the cross-spectral density function has a high magnitude with maximum coherence where the pressure spectral changes its slope.
通过具有中等雷诺数的受限湍流射流来模拟动脉狭窄远端的流场。壁面压力波动通过泊松方程与射流的动量波动相关。推导了一个格林函数以满足圆柱面上的边界条件。这使得泊松方程的解仅包含波动动量的体积积分,由源与传感器之间的相对距离加权。使用激光多普勒测速仪测量了射流中心线和剪切层中部的速度波动。沿轴向通过九个壁面安装的压力传感器阵列同时检测壁面压力波动。速度和压力波动之间的互相关表明,压力波动主要由具有对流速度的湍流涡旋通过引起,该对流速度是射流出口速度的函数。由通过的大尺度结构的频率定义的斯特劳哈尔数仅在非常靠近射流出口处是初始条件的函数。在更下游,初始条件的影响消失,斯特劳哈尔数接近一个常数,与射流雷诺数无关。由于轴向方向上加权函数的快速衰减,射流出口附近的源对再附着附近壁面压力波动的贡献相当微弱。然而,对于位于距传感器一个喷嘴直径范围内的源,互谱密度函数具有高幅值,在压力谱改变斜率处具有最大相干性。