کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
4452248 1620738 2015 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Development of a novel aerosol impactor utilizing inward flow from a ring-shaped nozzle
ترجمه فارسی عنوان
توسعه یک ضربه گیر هوا فشرده با استفاده از جریان داخلی از یک نازل حلقه
موضوعات مرتبط
مهندسی و علوم پایه علوم زمین و سیارات علم هواشناسی
چکیده انگلیسی

This study demonstrated the proof of the concept of a novel in-line real impactor with a ring-shaped nozzle for pre-separation of 16.4 μm particles in the aerodynamic diameter in ambient inlets with a flow rate of 1500 L/min. The design parameters of the impactor were selected considering the Stk50 for an impactor with a rectangular nozzle. The agreement of the numerical predictions with the experimental data in terms of collection efficiency supported our simulation approach to investigate the performance of the impactor with a ring-shaped nozzle in a turbulent flow regime. Furthermore, it was shown that the collection efficiency of our newly developed impactor can be improved by using an orifice between the inlet and the nozzle of the impactor through numerical predictions and experiments. The collection efficiency curve and Stk50 of an impactor with an orifice becomes respectively steeper and smaller than an impactor without an orifice.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of Aerosol Science - Volume 85, July 2015, Pages 1–9
نویسندگان
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