کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
7713007 | 1497424 | 2016 | 15 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Computing supersonic non-premixed turbulent combustion by an SMLD flamelet progress variable model
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
شیمی
الکتروشیمی
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Computing supersonic non-premixed turbulent combustion by an SMLD flamelet progress variable model Computing supersonic non-premixed turbulent combustion by an SMLD flamelet progress variable model](/preview/png/7713007.png)
چکیده انگلیسی
This paper presents a statistically more likely distribution (SMLD) approach for the evaluation of the presumed probability density function (PDF) in flamelet progress variable (FPV) models for non-premixed supersonic combustion. The numerical simulation of the NASA Langley Research Center supersonic H2-Air combustion chamber is performed using two approaches: the first one is a standard FPV model, built presuming the functional shape of the PDFs of the mixture fraction, Z, and of the progress parameter, Î; the second approach employs the SMLD technique to presume the joint PDF of Z and Î. The standard and FPV-SMLD models have been developed using the low Mach number assumption. In both cases, the temperature is evaluated by solving the total-energy conservation equation, providing a more suitable approach for the simulation of supersonic combustion. By comparison with experimental data, the proposed SMLD model is shown to provide a clear improvement with respect to the standard FPV model, especially in the auto-ignition and stabilization regions of the flame.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: International Journal of Hydrogen Energy - Volume 41, Issue 1, 5 January 2016, Pages 632-646
Journal: International Journal of Hydrogen Energy - Volume 41, Issue 1, 5 January 2016, Pages 632-646
نویسندگان
A. Coclite, L. Cutrone, M. Gurtner, P. De Palma, O.J. Haidn, G. Pascazio,