期刊文献+

贴体坐标系下离散坐标法计算尾喷焰辐射特性 被引量:21

Numerical modeling of infrared radiation properties of exhaust plume by the Discrete Ordinates Method in body-fitted coordinates
下载PDF
导出
摘要 在计算尾喷焰燃气组分、辐射物性的基础上,用贴体坐标系下的离散坐标法(DOM),研究了不同工况下尾喷焰的红外光谱辐射特性随飞行高度的变化特征,分析了介质的辐射物性对尾喷焰辐射特性的影响. 研究结果表明: 尾喷焰的辐射物性对尾喷焰辐射传输计算有很大的影响;在所考虑的工况下,与喷焰轴向垂直的方向上光谱辐射最强. The parameters of concentration and temperature distribution of particles and radiative parameters of gas phase molecular species are computed. The Discrete Ordinates Method in general body-fitted coordinates is used in investigating the relation between the radiation field of exhaust plume and flight altitude and Mach number, and the influence of media radiative properties on plume radiation is also analyzed. The results show that the media radiative properties intensively affect the exhaust plume radiation, for example, the particles scattering can smooth the radiative field in exhaust plume. Under the conditions described in the paper, the spectral radiative intensity vertical to axis is maximal.
出处 《上海理工大学学报》 CAS 北大核心 2003年第2期159-162,共4页 Journal of University of Shanghai For Science and Technology
基金 国家自然科学基金资助项目(50076010)
关键词 主动段 尾喷焰 红外辐射 离散坐标法 光谱特性 boosting stage exhaust plume infrared radiation Discrete Ordinates Method spectral properties
  • 相关文献

参考文献6

  • 1董土奎.[D].哈尔滨:哈尔滨工业大学,2002.
  • 2阮立明.[D].哈尔滨:哈尔滨工业大学,1997.
  • 3Baek S W, Kim M Y. Analysis of radiative heating of a rocket plume base with the finite volume method[J].lnt J of Heat Mass Transfer, 1997, 40(7): 1501-1508.
  • 4Vitkin E I. Physico-mathematical model of rocket exhaust plume[J]. J of Heat and Mass Transfer, 1997,40(5): 1227-1241.
  • 5Piesik E T. Aluminized propellants and a method defining low-altitued exhaust plume[J]. J Spacecraft,1986, 23(2): 215-221.
  • 6Ferziger J H, Peric M. Computational Methods for Fluid Dynamics[M]. Berlin: Springer, 1996.

同被引文献181

引证文献21

二级引证文献91

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部