Author/Authors :
Lei، نويسنده , , Zhang; Asgharian، نويسنده , , Bahman; Anjilvel، نويسنده , , Satish ، نويسنده ,
Abstract :
Particle deposition in symmetric bifurcating airways due to inertial
impaction was studied numerically for inspiratory Hows. Three-dimensional bifurcation
models were constructed. The models had different parent and daughter
diameters comparable to the airway generations 3~ of the human lung. Bifurcation
angles of the models were also varied (30°, 45°, and 60°). Airftow fields in the
models were obtained by a finite-element method (FIDAP, Fluid Dynamics International,
Evanston, It) for different Reynolds numbers of 100, 265, 530, and 1060
under parabolic and uniform inlet velocity conditions. The calculated How field data
were used to simulate particle trajectory in the airways. Particle deposition effi.
ciency was obtained using the limiting trajectory method. Inlet How velocity profile,
How Reynolds number, and bifurcation angle were found to have substantial effects
on particle deposition. Based on calculated deposition results, empirical equations
were derived for particle deposition efficiency as a function of nondimensional
parameters of Stokes number, Reynolds number, and bifurcation angle for a
parabolic or a uniform inHow. The proposed formulae compared favorably with
available experimental data and are applicable to a particle lung deposition model