Choi Sanghun, Choi Jiwoong, Lin Ching-Long
Department of Mechanical Engineering, Kyungpook National University, Daegu 41566, South Korea e-mail: .
IIHR-Hydroscience & Engineering, Iowa City, IA 52242; Department of Mechanical and Industrial Engineering, The University of Iowa, Iowa City, IA 52242 e-mail: .
J Biomech Eng. 2018 Jan 1;140(1):0110101-01101013. doi: 10.1115/1.4038163.
The aim of this study was to investigate and quantify contributions of kinetic energy and viscous dissipation to airway resistance during inspiration and expiration at various flow rates in airway models of different bifurcation angles. We employed symmetric airway models up to the 20th generation with the following five different bifurcation angles at a tracheal flow rate of 20 L/min: 15 deg, 25 deg, 35 deg, 45 deg, and 55 deg. Thus, a total of ten computational fluid dynamics (CFD) simulations for both inspiration and expiration were conducted. Furthermore, we performed additional four simulations with tracheal flow rate values of 10 and 40 L/min for a bifurcation angle of 35 deg to study the effect of flow rate on inspiration and expiration. Using an energy balance equation, we quantified contributions of the pressure drop associated with kinetic energy and viscous dissipation. Kinetic energy was found to be a key variable that explained the differences in airway resistance on inspiration and expiration. The total pressure drop and airway resistance were larger during expiration than inspiration, whereas wall shear stress and viscous dissipation were larger during inspiration than expiration. The dimensional analysis demonstrated that the coefficients of kinetic energy and viscous dissipation were strongly correlated with generation number. In addition, the viscous dissipation coefficient was significantly correlated with bifurcation angle and tracheal flow rate. We performed multiple linear regressions to determine the coefficients of kinetic energy and viscous dissipation, which could be utilized to better estimate the pressure drop in broader ranges of successive bifurcation structures.
本研究的目的是在不同分叉角度的气道模型中,研究并量化在不同流速下吸气和呼气过程中动能和粘性耗散对气道阻力的贡献。我们采用了直至第20代的对称气道模型,在气管流速为20升/分钟时具有以下五种不同的分叉角度:15度、25度、35度、45度和55度。因此,总共进行了十次吸气和呼气的计算流体动力学(CFD)模拟。此外,我们针对35度的分叉角度,对气管流速值为10和40升/分钟的情况进行了另外四次模拟,以研究流速对吸气和呼气的影响。使用能量平衡方程,我们量化了与动能和粘性耗散相关的压降贡献。发现动能是解释吸气和呼气时气道阻力差异的关键变量。呼气时的总压降和气道阻力大于吸气时,而吸气时的壁面剪应力和粘性耗散大于呼气时。量纲分析表明,动能系数和粘性耗散系数与代数密切相关。此外,粘性耗散系数与分叉角度和气管流速显著相关。我们进行了多元线性回归以确定动能和粘性耗散的系数,这些系数可用于在更广泛的连续分叉结构范围内更好地估计压降。