期刊文献+

物理化学模型对高温流场等离子体分布的影响 被引量:12

The effects of physicochemical models on distribution of plasma in high temperature flowfield
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摘要 开展飞行器高温流场等离子体分布数值模拟研究,对飞行器无线电通信系统设计具有重要意义。基于求解热化学非平衡N-S方程的数值方法,发展了复杂三维绕流等离子体数值模拟手段。利用电子数密度飞行测量数据,验证了数值模拟方法的可行性。研究了化学反应模型与热化学非平衡模型、壁面催化和壁面温度条件对流场等离子体分布模拟结果的影响,分析了升力体外形绕流等离子体的分布特性。研究表明:采用7组分与11组分化学反应模型对温度高达10000K的高温空气流场等离子体进行数值模拟,获得的电子数密度存在较大差异,此时模型中除了考虑NO+外,还必须考虑O+等离子的影响;壁面条件特别是壁面材料催化特性对壁面附近等离子体分布有较大影响,获取可靠的壁面材料催化与温度数据是准确模拟升力体绕流等离子体分布的先决条件。 It is important for the design of radio communication system to understand the plasma distribu- tion in high-temperature flowfield. A numerical method to simulate the complicated plasma flow field around a hypersonic flight vehicle is developed by solving the Navier-Stokes equations with thermo-chemieal non- equilibrium source terms. The method is validated by comparison of the distribution of electron number den- sities with flight experiment. The effects of chemical reaction and thermo-ehemical nonequilibrium models, the wall temperatures and catalytic activities on the computational results are studied. The distribution of plasma in flow over a lifting body are investigated too. The results show that the electron number densities computed by seven-species and eleven-species chemical model are different obviously when the flowfield tem- peratures beyond IO000K, and in the case 0+ must be taken into account in chemical reaction models besides NO+. The wall conditions, especially the catalytic activities, have a more important effect on the distribu- tion of plasma, the reliable data of the wall catalytic activities, have a more important effect on the distribu- tion of plasma, the reliable data the wall catalytic activities, have a more important effect on the distribution of plasma, the reliable data of the wall catalytic activities, have a more important on the distribution of plas- ma, the reliable data of the wall catalytic activities and temperatures must be obtained firstly in order to sim- ulate exactly the plasma flow over a lift body.
出处 《空气动力学学报》 CSCD 北大核心 2013年第5期541-545,553,共6页 Acta Aerodynamica Sinica
关键词 热化学非平衡 化学反应 等离子体 电子数密度 N—S方程 升力体 thermo-chemical nonequilibrium chemical reactions plasma electron number densities Navier-Stokes equations lift body
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参考文献14

  • 1MUYLAERT J, CIPOLLINI F, et al. In-flight research on real gas effects using the ESA EXPERT vehicles[R]. AIAA 2003-6981, 2003.
  • 2MORABITO D, KORNFELD R, et al. The mars phoenix communications brownout during entry into the martian atmosphere[R]. IPN Progress Report, 2009: 42-179.
  • 3HARTUNIAN R A, STEWART G E, et al. Implications and mitigation of radio frequency blackout during reentry of reusable launch vehicles [R]. AIAA 2007-6633, 2007.
  • 4MATHER D E, PASQUAL J M, SILLENCE J P. Ra- dio frequency (RF) blackout during hypersonic reentry [R]. AIAA 2005-3443. 2005.
  • 5STARKEY R P. Electromagnetic wave/magnetoactive plasma sheath interaction for hypersonic vehicle teleme- try blackout analysis[R]. AIAA 2003-4167, 2003.
  • 6SCALABRIN L C, BOYD I D. Numerical simulation of weakly ionized hypersonic flow for reentry configura- tions[R]. AIAA 2006-3773, 2006.
  • 7BLOTTNER F G . Viscous shock layer at the stagna- tion point with nonequilibrium air chemistry[J]. AIAA Journal, 1969, 7(12): 2281- 2288.
  • 8DUNN M G, KANG S W. Theoretical and experimental studies of reentry plasmas[R]. NASA-CR-2232, 1973.
  • 9GUPTA R N, YOS J M, et al. A review of reaction rates and thermodynamic and transport properties for an ll-species air model for chemical and thermal nonequi- librium calculations to 30000 K[R]. NASA-RP-1232, 1990.
  • 10LINT C, SPROUL L K, et al. Reentry plasma effects on electromagnetic wave propagation[R]. AIAA 95- 1942.

二级参考文献1

  • 1董维中.热化学非平衡效应对高超声速流动影响的数值计算与分析:[博士学位论文].北京:北京航空航天大学,1996..

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