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Numerical Simulation for Nasal Flow with Partial Inferior Turbinatomy - A Turbulent Model

机译:部分劣质汽轮瘤的鼻流量数值模拟 - 一种湍流模型

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Partial Inferior turbinectomy is typically performed for patients suffering from chronic nasal obstruction due to hypertrophy of inferior turbinates and are refractory to other more conservative treatments In this paper, the effects of the various manner of incision performed on the inferior turbinates in terms of the resulting nasal air flow pattern were analyzed using computational fluid dynamics (CFD). The three 3D nasal models with partial inferior turbinectomy were reconstructed from the MRI scans of a healthy human subject by simulating the three remaining shapes of inferior turbinate after the respective turbinate surgery with the use of the software MIMICS 12.1. Thereafter high resolution 3D volume meshes comprising boundary layer effects and computational domain exterior to the nose were constructed. Numerical simulations were carried out using FLUENTS for CFD simulations. The Reynolds averaged Navier-Stokes equations were solved for the turbulence flow with SST k-ω model. The consequences of the various types of turbinate surgery were compared with the originally healthy nasal model as well as the nasal model with severe nasal obstruction. The velocity streamlines, the total pressure drop through the nasal cavity, and the local wall shear stress distribution were presented. The existence of small vortices, relatively larger local velocity and wall shear stress showed that turbinate surgery should be carefully planned as it may affect normal local nasal functions.
机译:通常对患有慢性鼻梗阻的患者进行部分劣质突发术,由于脱浊鼻内肥大,并且在本文中对其他更保守的处理是难治性的,因此在所得到的鼻腔方面对各种切口进行各种切口的影响使用计算流体动力学(CFD)分析空气流动模式。通过使用软件模仿12.1,通过模拟各种鼻甲手术后的三种剩余鼻塞的MRI扫描来重建具有部分下湍流术的三维鼻模型。此后,构造了包括边界层效果的高分辨率3D容积网格和鼻子外部的计算域。使用流频对CFD模拟进行数值模拟。 Reynolds平均为Navier-Stokes方程求助于SST k-ω模型的湍流流程。将各种类型的鼻甲手术的后果与最初健康的鼻型以及具有严重鼻塞的鼻模进行进行比较。速度流动,通过鼻腔的总压降和局部壁剪切应力分布。小涡流的存在,相对较大的局部速度和壁剪切应力显示,应仔细策划鼻甲手术,因为它可能影响正常的局部鼻功能。

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