气体稀薄效应对热流计算的影响

陈杰; 张家骐; 欧吉辉

doi:10.7638/kqdlxxb-2019.0008

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气体稀薄效应对热流计算的影响

研究论文 | 更新时间：2026-05-28

- 气体稀薄效应对热流计算的影响
- Influence of rarefied gas effect on the computation of heat flux
- 空气动力学学报 2019年37卷第5期页码：691-697
- 作者机构：
  
  天津大学机械工程学院高速空气动力学研究室,天津,300072
- 作者简介：
  
  陈杰(1986-), 女, 甘肃人, 副研究员, 研究方向:稀薄气体动力学.E-mail:jie.chen@tju.edu.cn
- 基金信息：
  
  国家自然科学基金（11802202，11732011）
- DOI：10.7638/kqdlxxb-2019.0008
  中图分类号： V211.3
- 纸质出版：2019
- 稿件说明：
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陈杰, 张家骐, 欧吉辉. 气体稀薄效应对热流计算的影响[J]. 空气动力学学报, 2019, 37(5): 691-697.

CHEN Jie, ZHANG Jiaqi, OU Jihui. Influence of rarefied gas effect on the computation of heat flux[J]. 2019, 37(5): 691-697.
陈杰, 张家骐, 欧吉辉. 气体稀薄效应对热流计算的影响[J]. 空气动力学学报, 2019, 37(5): 691-697. DOI： 10.7638/kqdlxxb-2019.0008.

CHEN Jie, ZHANG Jiaqi, OU Jihui. Influence of rarefied gas effect on the computation of heat flux[J]. 2019, 37(5): 691-697. DOI： 10.7638/kqdlxxb-2019.0008.

摘要

临近空间高超声速飞行器的研发越来越受到关注。周恒和张涵信在《中国科学》上的《空气动力学的新问题》一文中分析了在此情况下现有的空气动力学的不足，其中之一就是需要考虑流场中可能出现的局部稀薄气体效应，并且针对临近空间高超声速飞行器边界层进行了详细的分析。陈杰和赵磊在此基础上研究了强剪切下的气体稀薄效应，给出了判别气体稀薄效应的无量纲参数

，并提出对传统连续介质模型中的黏性系数基于

参数进行修正。本文将通过类似的研究方法，采用DSMC（Direct Simulation Monte Carlo）研究纯导热问题中的气体稀薄效应，通过对粒子速度分布函数的分析提出了相应的刻画气体稀薄效应的参数

，获得了依赖参数

的导热系数修正规律，并进一步将该修正规律纳入CFD（Computational Fluid Dynamics）计算，验证了该算法对圆柱绕流问题表面热流预测的精度。

Abstract

Research and development of the technology for near space hypersonic flying vehicles have drawn more and more attention. In the article "New Problems of Aerodynamics"

Zhou and Zhang showed that

for near space flying vehicles

the existing aerodynamics is inadequate and one of the new problems is how to take the local rarefied gas effect into consideration. They also analysed hypersonic boundary layer of near space flying vehicles. Based on the research

Chen and Zhao studied the local rarefied gas effect for strong shear flow

and proposed a non-dimensional parameter

characterize the rarefied gas effect. They indicate that the viscosity coefficient in conventional continuum model should be modified according to the value of

. In this paper

in a similar way

the rarefied gas effect in heat conduction problem is investigated by Direct Simulation Monte Carlo (DSMC). A characteristic parameter

is proposed based on the analysis of the velocity distribution functions of molecules

and the correction on thermal conductivity depending on the parameter

is obtained. A hypersonic flow of argon over a two dimensional cylinder is simulated by the proposed model

and the heat flux on the surface is examined.

关键词

Keywords

references

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