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Non-invasive estimation of pressure changes along a streamline using vector velocity ultrasound

机译:使用载体速度超声沿着流线的压力变化的非侵入性估计

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A non-invasive method for estimating pressure changes along a streamline using ultrasound is presented. The suggested method estimates pressure gradients from 2-D vector velocity fields. Changes in pressure are derived using a model based on the Navier-Stokes equations. Scans of a carotid bifurcation phantom with a 70% constriction are performed using a linear array transducer connected to the experimental scanner, SARUS. 2-D fields of angle-independent vector velocities are acquired to a depth of 3 cm using directional synthetic aperture vector flow imaging. The performance of the suggested estimator is evaluated by comparing its results to a 3-D numerical simulation model. The study showed pressure drops across the constricted phantom varying from -5 Pa to 7 Pa with a standard deviation of 4%. The proposed method had a normalised root-mean-square error of 10% in reference to the simulation model. Further, an in-vivo scan of the carotid bifurcation is made to show the feasibility of the technique in a less experimental environment.
机译:提出了一种用于沿着使用超声波估计压力变化的非侵入性方法。建议的方法估计来自2-D矢量速度场的压力梯度。使用基于Navier-Stokes方程的模型导出压力的变化。使用连接到实验扫描仪的线性阵列换能器来执行具有70%收缩的颈动脉分叉幻影的扫描。使用方向合成孔径向量流量成像获取与角度无关矢量速度的2-D字段的3cm的深度。通过将其结果与三维数值模拟模型进行比较来评估建议的估计器的性能。该研究表明,在-5Pa至7Pa的限制幻影上显示压力下降,标准差为4%。所提出的方法在参考模拟模型中具有10%的归一化的根均方误差。此外,制备颈动脉分叉的体内扫描以显示该技术在较低的实验环境中的可行性。

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