کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
6973282 1453272 2015 5 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
A numerical approach to investigate the maximum permissible nozzle diameter in explosion by hot turbulent jets
ترجمه فارسی عنوان
یک رویکرد عددی برای بررسی حداکثر قطر نازل مجاز در انفجار با جت های شیب دار داغ
موضوعات مرتبط
مهندسی و علوم پایه مهندسی شیمی بهداشت و امنیت شیمی
چکیده انگلیسی
The ignition of a combustible environment by hot jets is a safety concern in many industries. In explosion protection concepts, for a protection of the type “flameproof enclosures” a maximum permissible gap is of major importance. In this work a numerical framework is described to investigate the ignition processes by a hot turbulent jet which flows out from such gaps. A Probability Density Function (PDF) method in conjunction with a reaction-diffusion manifold (REDIM) technique is used to model the turbulent reactive flow. In this paper the ignition of a stoichiometric mixture of hydrogen/air gas by a hot exhaust turbulent jet is examined. The impact of the nozzle diameter on the ignition delay time is investigated, too. The method is used to explore the maximum nozzle diameter for specific boundary conditions for which there is no ignition.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of Loss Prevention in the Process Industries - Volume 36, July 2015, Pages 539-543
نویسندگان
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