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下鼻甲肥大对湍流气流空气动力学模式和生理功能的影响 - 一种 CFD 模拟模型。

Impact of inferior turbinate hypertrophy on the aerodynamic pattern and physiological functions of the turbulent airflow - a CFD simulation model.

机构信息

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

出版信息

Rhinology. 2010 Jun;48(2):163-8. doi: 10.4193/Rhin09.093.

Abstract

INTRODUCTION

The aim of this study was to investigate the effects of nasal obstruction with enlargement of inferior turbinates on the aerodynamic flow pattern using Computational Fluid Dynamics (CFD) tools including the effects of turbulence.

METHODS

A high-resolution 3-dimensional model of the nasal cavity was constructed from MRI scans of a healthy human subject using MIMICS 12.0 software. Nasal cavities corresponding to healthy, moderate and severe nasal obstructions were simulated by enlarging the inferior turbinate geometrically. Numerical simulations with turbulent flow models were implemented using FLUENTS for CFD simulations.

RESULTS

In the healthy nose, the main respiratory air stream occurs mainly in the middle of the airway, accompanied by a diffused pattern of turbulent flow on the surface of the nasal mucosa. The peak value of turbulent flow is found in the functional nasal valve region. However, this aerodynamic flow pattern has partially or completely changed in the models with enlarged inferior turbinate. An inhalation flow rate of 34.8 L/min with a maximum velocity of 5.69 m/s, 7.39 m/s and 11.01 m/s are detected, respectively, in the healthy, moderately and severely obstructed noses. Both total negative pressure and maximum shear stress have increased by more than three and two times, respectively, in severely blocked noses compared to the healthy one.

CONCLUSION

Data of this study provide quantitative and quantitative information of the impact of inferior turbinate hypertrophy on the aerodynamic pattern and physiological functions of nasal airflow. By including the model of turbulent airflow, the results of this experimental study will be more meaningful and useful in predicting the aerodynamic effects of surgical correction of inferior turbinate hypertrophy.

摘要

引言

本研究旨在使用计算流体动力学(CFD)工具(包括湍流效应)研究下鼻甲肥大引起的鼻塞对空气动力学流动模式的影响。

方法

使用 MIMICS 12.0 软件,根据健康人体的 MRI 扫描构建了鼻腔的高分辨率三维模型。通过几何放大下鼻甲来模拟健康、中度和重度鼻塞的鼻腔。使用 FLUENTS 进行 CFD 模拟,实现了带有湍流模型的数值模拟。

结果

在健康的鼻腔中,主要呼吸气流主要发生在气道的中间,同时伴有鼻腔黏膜表面的弥散式湍流。湍流的峰值出现在功能性鼻阀区域。然而,在鼻甲增大的模型中,这种空气动力学流动模式已经部分或完全改变。在健康、中度和重度鼻塞的鼻腔中,分别检测到 34.8 L/min 的吸入气流速率,最大速度为 5.69 m/s、7.39 m/s 和 11.01 m/s。与健康鼻腔相比,严重鼻塞的鼻腔中的总负压和最大剪切力分别增加了三倍和两倍以上。

结论

本研究的数据提供了下鼻甲肥大对鼻腔气流动力学模式和生理功能影响的定量和定性信息。通过包括湍流气流模型,本实验研究的结果将更有意义和有用,可用于预测下鼻甲肥大手术矫正的空气动力学效应。

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