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再入飞行器驻点流光辐射特性的理论建模 被引量:1

THE THEORY MODEL FOR OPTICAL RADIATIONCHARACTERISTIC OF STAGNATIONREGION IN REENTRY PROCESS
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摘要 本文用直接模拟蒙特卡罗法,对再入体驻点区域的流场、光辐射特性进行了研究.针对头部锥体驻点区(包括激波层),建立了流场中的化学反应模型,中性粒子和等离子体的热运动、粒子间碰撞的理论模型,碰撞激发辐射和化学发光辐射的物理模型.给出了样本粒子运动方向和速率、粒子碰撞对的选择等蒙特卡罗法概率模型和计算方法. By means of the direct simulation Monte Carlo method, the flow-field and optical radiation characteristic of stagnation region in reentry process are calculated in this paper. Inthe stagnation region (including shock layer) at head of reentry vehicle, the chemical reaction model in flow field, thermal motion model of neutral particle and plasma body,collisionmodel among particles, the models of thermal exciting emitting and chemical irradiate areestablished. The MC probability model of moving direction, velocity of particles and that ofchoice of collision couple are given as well.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 1999年第6期720-724,共5页 Journal of Engineering Thermophysics
基金 国家杰出青年科学基金 国家自然科学基金
关键词 再入飞行器 驻点区 光辐射特性 流场分析 direct simulation Monte Carlo method, stagnation region, optical radiationcharacteristic
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  • 1徐南荣.喷气流红外辐射场的数值计算[J].航空学报,1995,16(6):647-653. 被引量:20
  • 2GUO Z,MARUYAMA S.Radiative heat transfer in inhomogeneous nongray and anistropically scattering media[J].International Journal of Heat and Mass Transfer,2000,43(13):2325-2336. 被引量:1
  • 3MORIZUMI S J,CARPENTER M J.Thermal radiation from the exhaust plume of an aluminized composite propellant rocket[J].Journal of Spacecraft and Rocket,1964,1(4):501-507. 被引量:1
  • 4LUDWIG C B,MALKMUS W,WALKER J.A theoretical model for absorbing,emitting and scattering plume radiation[C]//Horton T E.Spacecraft radative transfer and temperature control.New York:AIAA Progress Series in Astronautics and Aeronautics,1982:111-127. 被引量:1
  • 5PIESIK E T.Aluminized propellants and a method defining low-altitude exhaust plumes[J].Journal of Spacecraft and Rocket,1986,23(4):215-221. 被引量:1
  • 6SCUTARU D.Measurements and calculations of CO2 absorption at high temperature in the 4.3 μm and 2.7 μm regions[J].Journal of Quantitative Spectroscopy and Radiative Transfer,1993,50(2):179-191. 被引量:1
  • 7RUAN Liming,QI Hong,LIU Linhua,TAN Heping.The radiative transfer in cylindrical medium and partition allocation method by overlap regions[J].Journal of Quantitative Spectroscopy and Radiative Transfer,2004,86:343-352. 被引量:1
  • 8周学华.高超声速钝体尾流光电特性的计算[J].空气动力学学报,1992,10(2):255-260. 被引量:1
  • 9郝金波,董士奎,谈和平.固体火箭发动机尾喷焰红外特性数值模拟[J].红外与毫米波学报,2003,22(4):246-250. 被引量:18

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