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Received: 2007-02-10

Revision Accepted: 2007-04-17

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Journal of Zhejiang University SCIENCE A 2007 Vol.8 No.7 P.1053-1058

http://doi.org/10.1631/jzus.2007.A1053


Simulation of turbulent combustion in DLR Scramjet


Author(s):  ZOU Jian-feng, ZHENG Yao, LIU Ou-zi

Affiliation(s):  School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China

Corresponding email(s):   zoujianfeng@zju.edu.cn, liuouzi@hotmail.com

Key Words:  Scramjet, Turbulent combustion, Unstructured grid, Finite volume method


ZOU Jian-feng, ZHENG Yao, LIU Ou-zi. Simulation of turbulent combustion in DLR Scramjet[J]. Journal of Zhejiang University Science A, 2007, 8(7): 1053-1058.

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author="ZOU Jian-feng, ZHENG Yao, LIU Ou-zi",
journal="Journal of Zhejiang University Science A",
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pages="1053-1058",
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publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.2007.A1053"
}

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DOI - 10.1631/jzus.2007.A1053


Abstract: 
turbulent combustion in a DLR (German Aerospace Center) scramjet engine was simulated using the newly-proposed Partially Resolved Numerical Simulation (PRNS) procedure. The PRNS procedure uses temporal filtering to define large-scale turbulence, and the model developed to account for unresolved scales is grid independent. No problem about inner commutation error and inconsistencies will arise from the PRNS, while such issues are of concern in traditional Large Eddy Simulation (LES) methods. The mean results have good agreement with the experiment data and the flow structures with small scales are well resolved.

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

Reference

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[8] Oevermann, M., 2000. Numerical investigation of turbulent hydrogen combustion in a Scramjet using flamelet modeling. Aerospace Science and Technology, 4(7):463-480.

[9] Shih, T.H., Liu, N.S., 2004. Partially Resolved Numerical Simulation. AIAA Paper, No. 2004-0160.

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