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固体燃料冲压发动机内流物性参数自动计算
引用本文:陈军,武晓松,张家骅.固体燃料冲压发动机内流物性参数自动计算[J].推进技术,1999,20(6):32-35.
作者姓名:陈军  武晓松  张家骅
作者单位:1. 南京理工大学机械学院,南京,210094
2. 航天工业总公司31所,北京,100074
摘    要:通常固体燃料冲压发动机内流流动过程的模拟计算中,热力参数及输运系数都视作常数, 实际上, 它们随当地温度、组分等的改变而在发生变化。为确定热力参数和输运系数在各个截面上的变化规律, 研究了热力组分的平衡算法, 提供了简单实用的计算模型。计算结果显示, 把物性参数视作常数会带来较大误差, 说明了考虑物性参数在各个截面上的变化是非常必要的

关 键 词:固体燃料冲压发动机  物性参数~    输运系数~    流体动力学  计算流体力学

CALCULATION OF PHYSICS PERFORMANCE PARAMETERS OF INTERNAL FLOW FLUID FOR SFRJ
Chen Jun,Wu Xiaosong and Zhang Jiahua.CALCULATION OF PHYSICS PERFORMANCE PARAMETERS OF INTERNAL FLOW FLUID FOR SFRJ[J].Journal of Propulsion Technology,1999,20(6):32-35.
Authors:Chen Jun  Wu Xiaosong and Zhang Jiahua
Institution:The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074
Abstract:Usually thermodynamic and transportation parameters(such as ratio of specific heat,viscosity coefficient etc.)were treated as constants in numerical simulation of fluid of SFRJ.In fact,these parameters changed with local temperature, species etc.A simple but useful calculation model which determine thermodynamic and transportation parameters by equilibrium algorithm of thermodynamic species was presented.The results show that constant physical performance parameters can bring out considerable errors which illustrate that it is essential to consider the alternation of physical parameters at different area.
Keywords:Solid fueled ramjet  Physics performance parameters    Transporting coefficient    Fluid dynamics  Computational fluid dynamics  
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