Direct numerical simulation lifted hydrogen jet flame_ A priori study on combustion models.pdf
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Contents lists available at ScienceDirectActa Astronautica
Acta Astronautica 109 (2015) 52–64http://d
0094-57
n Corr
E-mjournal homepage: /locate/actaastroDirect numerical simulation of a supersonic lifted hydrogen jet
flame: A priori study on combustion models
Tai Jin a, Kun Luo a,n, Shuqiang Lu a,b, Jianren Fan a
a State Key Laboratory of Clean Energy Utilization, Zhejiang University, Hangzhou 310027, PR China
b Zhejiang Geely Automobile Research Institute Co., Ltd., Hangzhou, 310052, PR Chinaa r t i c l e i n f o
Article history:
Received 4 November 2014
Received in revised form
17 December 2014
Accepted 20 December 2014
Available online 29 December 2014
Keywords:
CMC submodels
Direct numerical simulation
Supersonic jet flame
Second-order closure
Taylor /10.1016/j.actaastro.2014.12.012
65/ 2014 IAA. Published by Elsevier Ltd. A
esponding author. Tel./fax: 86 571ail address: zjulk@ (K. Luo).a b s t r a c t
In this study, a systematic assessment of turbulent combustion submodels of conditional
moment closure (CMC) has been conducted using DNS data of a three-dimensional
spatially-developing supersonic lifted hydrogen flame with a Mach number of 1.2 at the
jet injection. It has been found that Beta pdf of mixture fraction can well capture the
mixing space of the high speed reacting flow. The linear model exhibits a good
performance for the axial velocity predictions. Girimajis model for scalar dissipation rate
performs well at upstream, while the AMC model presents better further downstream.
The first order closure for the conditional reaction rate deviates a lot from the DNS
extracted results. Second-order corrections made to temperature only or to the two rate-
limiting reaction steps induce improvement, still with much discrepancy. Second order
closure considering fluctuations of all the reacting species and temperature can accurately
reproduce the DNS results.
2014 IAA. Published by Elsevier Ltd. All rights reserved.1. Introduction
Renewed interests i
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