Factors Affecting Location of Nasal Airway Obstruction

Hui-fang Lin, Y. Hsieh, Yue-Lin Hsieh
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引用次数: 3

Abstract

A common cause of nasal airway obstruction (NAO) is nasal septum deviation (NSD). In clinical strategies, septoplasty has been one of the effective ways to resolve NAO. Current opinions on surgical removal of focal location and size remain inconclusive altogether. Studies on plethora demonstrated that pressure gradient (PG) or streamwise pressure gradient (SPG) are reliable predictors for the location or area of NAO. This study aims to investigate the physical quantities, i.e., pressure, vorticity and turbulent flow energy which are associated with NAO using computational fluid dynamics (CFD) and to provide aerodynamic characteristics of NAO in depth. Two patients were diagnosed with left-sided NSD using computed tomography (CT). The patient-specific three-dimensional (3D) nasal cavity model was reconstructed using Mimics 19.0 (Materialise, Belgium). We adopted the time-dependent k-ω model to predict the flow field. The transient Reynolds-Averaged Navier-Stokes equations were calculated using software COMSOL 5.5 (COMSOL Inc., Palo Alto, CA). The logistic regression method was implemented to evaluate the impact of the targeted physical quantities. The CFD results showed that the rotational flows and vortical flow structures emerged at the rear of the NAO site in the left nasal cavity. The magnitude of SPG, vorticity, and turbulent kinetic energy of the location of NAO was significantly larger than those of the contralesional side. Statistical analysis demonstrated that there was no statistical difference (p>0.05) among the vorticity, turbulent kinetic energy, and SPG. This study exhibits that the vorticity and turbulent kinetic energy (TKE) may also serve as effective aerodynamic markers for the prediction of NAO location besides PG and SPG. CFD with machine learning research assists physicians in handling nasal airway obstruction (NAO) patients' surgical sites in the future.
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影响鼻气道阻塞部位的因素
鼻腔导气管阻塞(NAO)的常见原因是鼻中隔偏曲(NSD)。在临床策略中,鼻中隔成形术是解决NAO的有效方法之一。目前关于手术切除病灶位置和大小的意见仍然没有定论。大量研究表明,压力梯度(PG)或流向压力梯度(SPG)是NAO位置或面积的可靠预测因子。本研究旨在利用计算流体动力学(CFD)研究与NAO相关的物理量,即压力、涡度和湍流能量,并深入提供NAO的气动特性。2例患者通过计算机断层扫描(CT)诊断为左侧NSD。使用Mimics 19.0 (Materialise, Belgium)重建患者特定的三维(3D)鼻腔模型。我们采用随时间变化的k-ω模型来预测流场。使用COMSOL 5.5软件(COMSOL Inc., Palo Alto, CA)计算瞬态reynolds - average Navier-Stokes方程。采用logistic回归方法评价目标物理量的影响。CFD结果表明,在左鼻腔NAO部位后部出现了旋转流动和旋涡流动结构。NAO位置的SPG、涡度和湍流动能的大小明显大于对侧。统计分析表明,涡度、湍流动能和SPG之间无统计学差异(p>0.05)。研究表明,涡度和湍流动能(TKE)也可作为预测NAO位置的有效气动指标。基于机器学习的CFD研究有助于医生在未来处理鼻气道阻塞(NAO)患者的手术部位。
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