Lattice Boltzmann Simulation of Droplet Collision Dynamic Using Index Function Model
محل انتشار: هفتمین کنفرانس دانشجویی مهندسی مکانیک
سال انتشار: 1392
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 1,081
فایل این مقاله در 6 صفحه با فرمت PDF قابل دریافت می باشد
- صدور گواهی نمایه سازی
- من نویسنده این مقاله هستم
استخراج به نرم افزارهای پژوهشی:
شناسه ملی سند علمی:
ASCME07_250
تاریخ نمایه سازی: 4 اسفند 1392
چکیده مقاله:
The phenomenon of binary droplet collision is of fundamental importance in the studies of raindrop formation, spraying processes, dispersed phase systems,and so on. Therefore, many investigations of the binary droplet collision dynamics have been performed by using experimental, numerical, and theoreticalapproaches. In this way, we simulated and studied binary droplet collision using Lattice Boltzmann twophase flow (index function model) method. LBM is anew compromising method with excellent features in two-phase modeling. Index function model which recently is presented by He, is a reliable model utilizedin this simulation. Accuracy of the model is examined by well-known basic analytical two-phase flowsincluding Laplace law and relaxation of rectangular cylinder, and our results are in good agreement with analytical outcomes which certify our final resultsquality. Two droplet collisions are simulated in different collision position such as: two equal droplets, two unequal droplets, direct collision, and offset collision.The density ratio of the liquid to the gas is fixed at 30. We used non-dimensional numbers (Reynolds, Weber) for considering different collision features (speed,viscosity force, surface tension, etc.). Binary droplet collision would result different behavior in new formeddroplet. Change in fluid specification and collision situation left various formation dynamics in new droplet. Results in variety of conditions are analyzedand compared with each other. Besides all analysis accuracy and ability of index function model for twophase flow problems is proved.
کلیدواژه ها:
نویسندگان
Majid Haghshenas
Aerospace Department, Sharif University of Technology, Tehran, Iran
Mohammad Taeibi-Rahni
Aerospace Department, Sharif University of Technology, Tehran, Iran
Mohammad-Reza Salimi
Aerospace Department, Sharif University of Technology, Tehran, Iran
مراجع و منابع این مقاله:
لیست زیر مراجع و منابع استفاده شده در این مقاله را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود مقاله لینک شده اند :