局部下鼻甲切开术鼻流的数值模拟-湍流模型

Xiao Bing Chen, H. Lee, V. Chong, D. Wang
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引用次数: 3

摘要

下鼻甲部分切除术是由于下鼻甲肥大引起的慢性鼻塞患者的典型手术,其他保守的治疗方法难以治疗。本文利用计算流体动力学(CFD)分析了不同切口方式对下鼻甲鼻腔气流模式的影响。通过使用MIMICS 12.1软件模拟下鼻甲手术后剩余的三种形状,根据健康受试者的MRI扫描重建三个部分切除下鼻甲的3D鼻模型。在此基础上,构建了包含边界层效应和鼻鼻外计算域的高分辨率三维体网格。采用FLUENTS进行数值模拟。用SST k - ω模型求解了湍流流场的Reynolds平均Navier-Stokes方程。将不同鼻甲手术方式与原健康鼻模型及重度鼻塞鼻模型进行比较。给出了速度流线、通过鼻腔的总压降和局部壁面剪应力分布。小漩涡的存在,相对较大的局部速度和壁剪切应力表明鼻甲手术应仔细计划,因为它可能影响正常的局部鼻功能。
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Numerical simulation for nasal flow with partial inferior turbinatomy-a turbulent model
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.
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