Fei D Y, Billian C, Rittgers S E
Biomedical Engineering Program, Virginia Commonwealth University, Richmond 23298.
Ultrasound Med Biol. 1988;14(1):21-31. doi: 10.1016/0301-5629(88)90160-3.
A model of the human carotid artery bifurcation has been constructed and tested under mean physiologic flow conditions (fluid viscosity = 0.035 poise; mean Re inlet = 400; unconstricted flow split = 70:30, internal carotid artery:external carotid artery). Smooth, axisymmetric constrictor plugs with 0, 20, 40, 60, and 80% diameter reduction are placed in the simulated proximal internal carotid artery to provide a range of flow conditions similar to those found clinically. Axial velocity measurements are made at sites +/- 0.625 radius within the lumen of the tube at distances of 0, 1, 3, 5 and 10 diameters downstream of the constrictor throat using H2 bubble markers and a 7.5 MHz ultrasound pulse Doppler. Measurement of mean, mode -3 dB down high and low and -9 dB down high and low velocities are made from selected fast-Fourier transform (FFT) spectra. The flow field downstream of the 0% diameter reduction is entirely laminar, exhibiting a peak skewed toward the flow divider along the entire 10 diameters downstream and having a consistently narrow bandwidth. Obstruction of the flow channel produces increased axial velocity at the constrictor (20%), an oscillatory jet extending approximately 5 diameters downstream (40%), a transitional jet extending approximately 5 diameters downstream (60%) and a turbulent jet extending approximately 3 diameters downstream (80%). Velocity bandwidth (both -3 dB and -9 dB) increases with degree of constriction and low velocity flow patterns exist between the center line and both tube walls. Presence of constriction produces characteristic downstream flow patterns which are distinctive for each degree of diameter reduction.
已经构建了一个人体颈动脉分叉模型,并在平均生理流动条件下(流体粘度 = 0.035泊;平均入口雷诺数 = 400;未收缩时的血流分配为70:30,即颈内动脉:颈外动脉)进行了测试。将直径分别减小0%、20%、40%、60%和80%的光滑轴对称收缩塞放置在模拟的颈内动脉近端,以提供一系列与临床情况相似的流动条件。使用H2气泡标记和7.5MHz超声脉冲多普勒仪,在收缩器喉部下游0、1、3、5和10个管径处的管腔内,在距中心线±0.625半径的位置进行轴向速度测量。从选定的快速傅里叶变换(FFT)频谱中测量平均速度、模式-3dB下的高低速度以及-9dB下的高低速度。直径减小0%时下游的流场完全是层流,在下游整个10个管径范围内,峰值偏向分流器,并且带宽始终很窄。流动通道的阻塞会使收缩器处的轴向速度增加(20%),产生一个向下游延伸约5个管径的振荡射流(40%),一个向下游延伸约5个管径的过渡射流(60%)和一个向下游延伸约3个管径的湍流射流(80%)。速度带宽(-3dB和-9dB)随收缩程度增加而增大,并且在中心线与管壁之间存在低速流动模式。收缩的存在会产生特征性的下游流动模式,每种直径减小程度的模式都不同。