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首页> 外文期刊>Rhinology >Aerodynamic effects of inferior turbinate surgery on nasal airflow--a computational fluid dynamics model.
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Aerodynamic effects of inferior turbinate surgery on nasal airflow--a computational fluid dynamics model.

机译:下鼻甲手术对鼻气流的空气动力学影响-一种计算流体动力学模型。

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摘要

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.
机译:背景:保守治疗失败时,可能需要进行鼻甲缩小手术,以减少鼻甲增大。这项研究的目的是使用计算流体力学(CFD)模拟评估下鼻甲手术对鼻部空气动力学的影响。方法:针对正常鼻子,扩大的下鼻甲和以下三个手术步骤进行了CFD模拟:(1)切除下鼻甲的下第三自由边缘,(2)切除下鼻甲的头部,以及(3)根治性下鼻甲切除术。这些模型是通过对健康人的MRI扫描建立的,并将湍流模型用于数值模拟。将这三个鼻甲手术的后果与最初健康的鼻腔模型以及严重鼻塞的模型进行了比较。结果:在正常鼻子中,大部分流线以相对涡旋自由流动的方式穿过与下鼻甲和中鼻甲相邻的普通鼻道。当下鼻甲增大时,流线以较高的速度指向上方,并增加了鼻咽部的壁切应力。在模拟的三种外科手术技术中,下三分之一切除后,壁切应力和鼻内压力达到了接近正常水平。此外,气流流线和湍流得到了改善,尽管它没有恢复到正常状态。如预期的那样,彻底的鼻甲切除术导致了先前CFD研究中证实的鼻内萎缩性鼻炎的空气动力学。结论:几乎没有证据表明根治性鼻甲手术后适当调节了吸入的空气。肥大性鼻甲的部分减少可改善鼻部空气动力学,这在切除下三分之一后最为明显。结果是基于单个个体的,如果没有其他主题的类似研究,则不能将其推广。

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