کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
761245 1462687 2015 12 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Passive scalar mixing in Mc <1 planar shear layer flows
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مکانیک محاسباتی
پیش نمایش صفحه اول مقاله
Passive scalar mixing in Mc <1 planar shear layer flows
چکیده انگلیسی


• We investigate the passive scalar mixing in supersonic planar shear layers.
• The defined mixing efficiency decreases with increasing density ratio.
• The mixing efficiency increases with increasing velocity ratio.
• The mixing efficiency decreases with increasing convection Mach number.

We investigate passive scalar mixing in spatially developing supersonic shear layer flows formed by two planar streams by means of large eddy simulation. After validation of the numerical procedures employing a high-order hybrid WENO/compact scheme by comparing the results of simulation with the results obtained from a well characterized experimental case, the effects of the convective Mach number, Mc, flow velocity ratio, r = U1/U2, and fluid density ratio, s = ρ1/ρ2, between Stream 1 and Stream 2 on passive scalar mixing are considered by examining the variation of mixing layer thickness and the mixing efficiency represented by the transport of the passive scalar. Mc is specified from 0.2 to 0.8. The evolution of large-scale coherent structures is well reproduced, with vortices undergoing rolling up, pairing, merging, and breaking up. The mixing layer thickness and mixing efficiency both decrease as Mc increases. As s increases, the mixing layer thickness increases, and the mixing efficiency of an entrained fluid decreases. As r increases, the mixing layer thickness decreases while the mixing efficiency increases. While the present results are not applicable to the examination of micro-mixing properties, which require assessment by experimental methods or high computing cost direct numerical simulation, they are useful for evaluating the effects of different flow parameters on macro-performance, which is equally important for scramjet combustor design and evaluation in engineering.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Computers & Fluids - Volume 123, 21 December 2015, Pages 32–43
نویسندگان
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