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下鼻甲手术对鼻气流的空气动力学影响——计算流体动力学模型。

Aerodynamic effects of inferior turbinate surgery on nasal airflow--a computational fluid dynamics model.

机构信息

Department of Mechanical Engineering, Faculty of Engineering. National University of Singapore, Singapore.

出版信息

Rhinology. 2010 Dec;48(4):394-400. doi: 10.4193/Rhino09.196.

Abstract

BACKGROUND

Turbinate reduction surgery may be indicated for inferior turbinate enlargement when conservative treatment fails. The aim of this study was to evaluate the effects of inferior turbinate surgery on nasal aerodynamics using computational fluid dynamics (CFD) simulations.

METHODS

CFD simulations were performed for the normal nose, enlarged inferior turbinate and following three surgical procedures: (1) resection of the lower third free edge of the inferior turbinate, (2) excision of the head of the inferior turbinate and (3) radical inferior turbinate resection. The models were constructed from MRI scans of a healthy human subject and a turbulent flow model was used for the numerical simulation. The consequences of the three turbinate surgeries were compared with originally healthy nasal model as well as the one with severe nasal obstruction.

RESULTS

In the normal nose, the bulk of streamlines traversed the common meatus adjacent to the inferior and middle turbinate in a relatively vortex free flow. When the inferior turbinate was enlarged, the streamlines were directed superiorly at higher velocity and increased wall shear stress in the nasopharynx. Of the three surgical techniques simulated, wall shear stress and intranasal pressures achieved near-normal levels after resection of the lower third. In addition, airflow streamlines and turbulence improved although it did not return to normal conditions. As expected, radical turbinate resection resulted in intra-nasal aerodynamics of atrophic rhinitis demonstrated in previous CFD studies.

CONCLUSION

There is little evidence that inspired air is appropriately conditioned following radical turbinate surgery. Partial reduction of the hypertropic turbinate results in improved nasal aerodynamics, which was most evident following resection of the lower third. The results were based on a single individual and cannot be generalised without similar studies in other subjects.

摘要

背景

当下鼻甲肥大经保守治疗无效时,鼻甲缩小手术可能是指征。本研究旨在使用计算流体动力学(CFD)模拟评估下鼻甲手术对鼻空气动力学的影响。

方法

对正常鼻腔、下鼻甲肥大和以下三种手术:(1)下鼻甲下缘三分之一游离缘切除术,(2)下鼻甲头部切除术和(3)下鼻甲根治性切除术进行 CFD 模拟。模型由健康人体 MRI 扫描构建,并使用湍流模型进行数值模拟。将三种鼻甲手术的后果与原始健康鼻模型以及严重鼻塞模型进行了比较。

结果

在正常鼻腔中,大部分流线在相对无涡的流动中穿过中下鼻甲附近的共同鼻道。当下鼻甲增大时,流线向上指向更高的速度,增加了鼻咽部的壁面剪切应力。在所模拟的三种手术技术中,下鼻甲的三分之一切除后,壁面剪切应力和鼻腔内压力接近正常水平。此外,虽然没有恢复到正常状态,但气流流线和湍流得到了改善。正如预期的那样,根治性鼻甲切除术导致了先前 CFD 研究中萎缩性鼻炎的鼻腔内空气动力学改变。

结论

根治性鼻甲手术后,吸入的空气几乎没有得到适当的调节。肥大鼻甲的部分缩小会改善鼻腔空气动力学,在下鼻甲下缘三分之一切除后最为明显。结果基于单个个体,在其他受试者中没有类似研究的情况下不能推广。

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