Department of Mechanical Engineering, Konkuk University, Seoul 143-701, Republic of Korea.
Respir Physiol Neurobiol. 2012 Mar 15;180(2-3):289-97. doi: 10.1016/j.resp.2011.12.005. Epub 2011 Dec 30.
Knowledge of airflow characteristics in the nasal cavity is essential to understanding the physiologic and pathologic aspects of nasal breathing. Airflows inside post-surgery models were investigated both experimentally and numerically to simulate the inferior turbinectomy. The left cavities of all three models are normal and right cavity is modified by (1) excision of the head of the inferior turbinate, (2) resection of the lower fifth of the inferior turbinate, and (3) resection of almost the entire inferior turbinate. Thin-slice CT (computed tomography) data (0.6mm deep) and meticulous refinement of the model surface by over a decade-long collaboration between engineers and an experienced ENT doctor resulted in the creation of sophisticated nasal cavity models. After numerical experiments and validation by comparison with the PIV results, the CFD code using the Reynolds stress turbulent model and variable temperature boundary condition on the mucosal wall was chosen as the proper numerical framework. Both global quantities (pressure drop, flow rate ratio, total wall heat transfer) and local changes (velocity, temperature, humidity, pressure gradient, and wall shear stress) were numerically investigated. The turbinectomy obviously altered the main stream direction. The flow rate in the upper airway near the olfactory slit decreased in models (1) and (3). This may weaken the olfactory function of the nose. Fluid and thermal properties that are believed to be related with physiology and prognosis are dependent on turbinate resection volume, position, and manner. Widening of the inferior airway does not always result in decreased flow resistance or wall heat transfer. The gains and losses of inferior turbinectomy were considered by analysis of the post-surgery model results. Nasal resistance was increased in model (1) due to sudden airway expansion. Nasal resistance increased and the wall heat transfer decreased in model (3) due to sudden airway expansion and excessive reduction of the mucosal wall surface area. Local shear stress and pressure gradient levels were increased in models (1) and (3).
鼻腔内气流特性的知识对于理解鼻腔呼吸的生理和病理方面至关重要。通过实验和数值模拟研究了手术后模型内的气流,以模拟下鼻甲切除术。所有三个模型的左鼻腔均正常,而右鼻腔则通过以下三种方式进行了修改:(1)切除下鼻甲头部;(2)切除下鼻甲的下五分之一;(3)切除几乎整个下鼻甲。通过工程师和一位经验丰富的耳鼻喉科医生十多年的合作,获得了薄层 CT(计算机断层扫描)数据(0.6 毫米深)并对模型表面进行了精细的改进,从而创建了复杂的鼻腔模型。经过数值实验并通过与 PIV 结果的比较进行验证后,选择了使用雷诺应力湍流模型和可变粘膜壁温度边界条件的 CFD 代码作为合适的数值框架。对全局量(压降、流量比、总壁传热)和局部变化(速度、温度、湿度、压力梯度和壁剪切应力)进行了数值研究。鼻甲切除术明显改变了主流方向。在模型(1)和(3)中,嗅缝附近的上气道中的流量减少。这可能会削弱鼻子的嗅觉功能。被认为与生理和预后相关的流体和热特性取决于鼻甲切除的体积、位置和方式。下气道的加宽并不总是导致流动阻力或壁传热的降低。通过对手术后模型结果的分析,考虑了下鼻甲切除术的得失。由于气道突然扩张,模型(1)中的鼻腔阻力增加。由于气道突然扩张和粘膜壁表面积过度减少,模型(3)中的鼻腔阻力增加,壁传热减少。模型(1)和(3)中的局部剪切应力和压力梯度水平增加。