Burleson A C, N'Guyen T, Fontaine A, Levine R A, Yoganathan A P
Cardiovascular Fluid Mechanics Laboratory, School of Chemical Engineering, Georgia Institute of Technology, Atlanta 30332-0100, USA.
Ultrasound Med Biol. 1995;21(7):899-911. doi: 10.1016/0301-5629(95)00035-p.
A technique is proposed for the noninvasive quantification of regurgitant flows under confined and impinging conditions. Its use requires only the knowledge of the jet orifice velocity, receiving chamber diameter, orifice-to-end wall distance and any downstream jet centerline velocity at a known distance from the orifice. The technique is based on dimensional analysis and provides a prediction of peak regurgitant flow rates. To validate the technique, known physiologic pulsatile flows were pumped through 2- and 4-mm circular orifices at 70 to 150 beats/min, into two different receiving chambers of 51 and 88 mm in diameter. At each heart rate, the peak orifice velocity was varied from 2 to 5 m/s, and the orifice-to-end wall distance was varied from 30 to 93 mm. Centerline velocities were recorded by pulsed Doppler ultrasound and averaged over multiple beats. A dimensional analysis of the parameters of the study provided an equation relating normalized centerline velocity to orifice-to-end wall distance, chamber diameter and downstream location. Statistical modeling of the experimental data was performed to compute the constants involved in this equation. The estimated (i.e., predicted by the technique) peak regurgitant flow rates were found to fall within 10% of the actual values, when centerline velocities were measured over a range of centerline distances from six orifice diameters to 85% of the chamber length. Therefore, the proposed technique provides, for the first time, a quantitative method for calculating valvular regurgitant flow rates under confined and impinging conditions.
本文提出了一种用于在受限和冲击条件下对反流流量进行无创定量分析的技术。该技术的应用仅需知晓射流孔口速度、接收腔直径、孔口到端壁的距离以及在距孔口已知距离处的任何下游射流中心线速度。该技术基于量纲分析,可预测反流峰值流量。为验证该技术,将已知的生理性脉动流以70至150次/分钟的频率通过2毫米和4毫米的圆形孔口,泵入直径分别为51毫米和88毫米的两个不同接收腔中。在每个心率下,孔口峰值速度在2至5米/秒之间变化,孔口到端壁的距离在30至93毫米之间变化。通过脉冲多普勒超声记录中心线速度,并在多个心动周期上进行平均。对研究参数进行量纲分析得到了一个将归一化中心线速度与孔口到端壁距离、腔室直径和下游位置相关联的方程。对实验数据进行统计建模以计算该方程中涉及的常数。当在从六个孔口直径到腔室长度的85%的一系列中心线距离上测量中心线速度时,发现估计的(即由该技术预测的)反流峰值流量落在实际值的10%以内。因此,所提出的技术首次提供了一种在受限和冲击条件下计算瓣膜反流流量的定量方法。