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首页> 外文期刊>AIAA journal >Numerical simulation of shock-enhanced mixing in nonuniform density turbulent jets
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Numerical simulation of shock-enhanced mixing in nonuniform density turbulent jets

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摘要

A numerical study of the interaction of weak normal shock waves with turbulent jets was conducted. The configuration consisted of a planar jet of air, helium, or carbon dioxide situated on the centerline of a shock tube with an air coflow. The shock strengths were M-s = 1.2 and 1.4. The numerical model was based on a time-dependent, Navier-Stokes approach and a two-equation q-omega turbulence model. The results indicate that passage of a shock through low-density (helium) jets produces a vortexlike structure not seen for the case of the air or carbon dioxide jets. Helium jets exhibit a decrease in mean jet fluid concentration due to shock interaction of up to approximately 30 at a location 30 jet exit heights downstream of the jet exit for a shock strength of M-s = 1.4. The amount of mixing enhancement increases with increasing shock strength and decreases with increasing downstream distance. In comparison, the air and carbon dioxide jets show a significantly smaller degree of mixing enhancement. These results are qualitatively consistent with recent experimental results in axisymmetric, turbulent jets subject to normal shock passage. References: 28

著录项

  • 来源
    《AIAA journal》 |2000年第11期|2113-2119|共7页
  • 作者

    Obata S.; Hermanson JC.;

  • 作者单位

    Natl Def Acad, Dept Aerosp Engn, 1-10-20 Hashirimizu, Kanagawa 2398686, Japan.;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 英语
  • 中图分类 航空、航天;航空;
  • 关键词

    Waves; Light;

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