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Applying Computational Fluid Dynamics Methods on Nasal Flow Investigations Based on a Real Domain Generated from CT Data

机译:基于CT数据实域的计算流体动力学方法在鼻腔流动研究中的应用

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Modern nasal surgery raises questions on the improvement of nasal airways, providing a patient with healthy, comfortable breathing. In fact, presently available and realizable measurements are not sufficient to define standard shapes for optimized flow behavior. Airway shapes determine local flow velocities and the degree of turbulence. Transition areas between laminar and turbulent flow regions affect particle transport and consequently the sensation of smell.Numerical simulation approaches (Computational Fluid Dynamics/CFD), particularly Large Eddy Simulation (LES), might help to understand the flow behavior of such complex geometries. Present clinical scanning techniques, e.g. CT, allow digital reconstructions of a patient's nasal geometry. These can be used to construct a simulation grid spanning the air flow domain required for breath flow calculations. From this point, investigations of varying geometries seem easy to realize. Even virtual surgery rooms with the aid of CFD seem possible.Within this interdisciplinary contribution, the principal steps for setting up such simulations will be outlined and compared to the steps taken within this project. Exemplary flow calculations based on a real nasal geometry will be shown, using a parallelized, compressible Navier-Stokes code. Applicability and limitations of this approach will be outlined. Focus is laid on questions related to grid generation/dependence and data validity.
机译:现代的鼻外科手术提出了关于改善鼻气道的问题,这为患者提供了健康舒适的呼吸。实际上,当前可用和可实现的测量不足以定义用于优化流动行为的标准形状。气道形状决定了局部流速和湍流程度。层流和湍流区域之间的过渡区域影响颗粒的运输,从而影响嗅觉。 数值模拟方法(计算流体力学/ CFD),特别是大涡模拟(LES),可能有助于了解这种复杂几何形状的流动行为。目前的临床扫描技术,例如CT可以对患者的鼻腔几何形状进行数字重建。这些可用于构建模拟网格,该网格跨越呼吸流量计算所需的气流域。从这一点出发,对各种几何形状的研究似乎很容易实现。甚至在CFD的帮助下虚拟手术室似乎也是可能的。 在这一跨学科的贡献中,将概述建立此类模拟的主要步骤,并将其与本项目中采取的步骤进行比较。将使用并行化的可压缩Navier-Stokes代码显示基于真实鼻腔几何形状的示例性流量计算。将概述这种方法的适用性和局限性。重点放在与网格生成/依赖性和数据有效性有关的问题上。

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