期刊文献+

硅基材料烧蚀产物对高温气体流场辐射影响 被引量:2

Effects of ablation products of silicon-based materials on radiation of high-temperature gas flow field
下载PDF
导出
摘要 高温气体流场辐射特性在高超声速飞行器目标探测、识别和气动热环境预测等方面具有重要应用。基于带辐射模型,考虑硅基防热材料热化学烧蚀产物的可见光和红外辐射机制,建立了烧蚀产物光谱参数的计算方法,发展了高温气体烧蚀流场辐射特性计算软件。高温气体烧蚀流场的数值模拟结果,利用所发展的辐射计算软件,计算分析了自由飞弹道靶实验模型及高超声速钝头体流场的辐射特性,重点研究了各种烧蚀产物的影响。研究表明:烧蚀产物对流场红外辐射特性具有重要影响。 The radiation characteristics of high-temperature gas flow have important application in detection, discrimination and aerothermal environment prediction for hypersonic vehicles. Based on a band model and considering the visible and infrared radiation of the ablation products of silicon-based materials for heat-shield, the method and code were developed to compute spectral parameter of ablation products and the radiation characteristics of high temperature gas flow field. The flow field parameters resulted from the numerical simulation and used the code, the radiation characteristics of flow over a model in a free-flight ballistic range and hypersonic blunt body were computed, and particularly the ablation effects were studied. The research shows that the ablation products have important effects on infrared radiation of the flow field.
出处 《红外与激光工程》 EI CSCD 北大核心 2015年第1期42-47,共6页 Infrared and Laser Engineering
基金 国家自然科学基金(91216204)
关键词 高超声速飞行器 硅基材料 流场 高温气体 烧蚀产物 辐射特性 hypersonic vehicles silicon-based materials flow field high-temperature gas ablation products radiation characteristics
  • 相关文献

参考文献13

  • 1范晋祥,杨建宇.红外成像探测技术发展趋势分析[J].红外与激光工程,2012,41(12):3145-3153. 被引量:84
  • 2孙成明,袁艳,黄锋振,王潜.空间目标红外成像特性建模与仿真[J].红外与激光工程,2012,41(3):563-568. 被引量:17
  • 3Park C. Nonequilibrium air radiation (NEQAIR) program: User's Manual[S]//NASA-TM, 1985: 86707.
  • 4Ludwig C B, Malkmus W, Rcardon J E,et al. The standard infrared radiation model[C]//AIAA, 1981, 81: 1051.
  • 5Hartung L C. Predicting trermochemical nonequilibrium manual for the LORAN Memorandum, 1994: 4564. radiative heat transfer in flow field. Theory and user's code [C]//NASA Technical.
  • 6张志成,高铁锁,董维中,许勇,国义军.再入飞行器目标特性建模研究[J].实验流体力学,2007,21(1):7-12. 被引量:10
  • 7Laux C O, Gessman R J, Hilbert B, et al. Experimental study and modeling of Infrared Air plasma radiation [C]// AIAA, 1995, 95: 2124.
  • 8Levin D A, Candler G V, Limbaugh C C, et al. Multi- spectral Shock layer radiance from a hypersonic slender body [C]//AIAA, 1999, 99: 3747.
  • 9Clemente M D, Ferrarella D. Convective and radiative heat flux estimation on a re-entry capsule[C]// AIAA,2010:5067.
  • 10Laux, C O, Winter M, Merrifield J, et al. Influence of ablation products on the radiation at surface of a blunt hypersonic vehicle at 10km/s[C]//AIAA, 2009: 3925.

二级参考文献38

  • 1彭华峰,陈鲸,张彬.天基光电望远镜对空间目标成像的模拟[J].光电工程,2005,32(10):14-17. 被引量:18
  • 2杭建,林贞彬,郭大华,林建民,曾明,黄德,葛学真.高焓风洞中钝体近尾流红外辐射测试技术[J].实验流体力学,2005,19(4):69-73. 被引量:2
  • 3周晓东,郭明.空间目标动态红外图像的计算机生成[J].红外与激光工程,2007,36(1):5-8. 被引量:18
  • 4BLOTTNER F G. Prediction of electron density in the boundary layer on entry vehicles with ablation [R]. N71-21113 , 1971.
  • 5GUPTA R, LEE K, MOSS J, et al. Viscous-shock-layer solution with coupled radiation and ablation injection for earth entry[R]. AIAA 90-1697.
  • 6BHUTTA B A, LEWIS C H. A new technique for low- to high altitude predictions of ablative hypersonic flow- fields[R]. AIAA 91-1392.
  • 7KEENAN J A, CANDLER G V. Simulation of graphite ablation and oxidation under re-entry conditions [R]. AIAA 94-2083.
  • 8PARK C, JAFFE R L, PARTRIDGE H. Chemical-kinetic parameters of hyperbolic earth entry[J]. Journal of Thermodynamics and Heat Transfer, 2001, 15 ( 1 ) : 76-90.
  • 9DONG W Z, GAO T S. Numerical simulation of ablative flowfields over a hypersonic re-entry blunt body [R]. Proceedings of the Fourth Asia Workshop on CFD [C]. Tokyo, Japan, 2004:203-208.
  • 10王苏.再入条件下气相反应过程研究[R].北京:中国科学院力学研究所,2007.

共引文献117

同被引文献12

引证文献2

二级引证文献6

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