高速双锥绕流中热化学与输运模型影响研究
EFFECTS OF THERMOCHEMICAL AND TRANSPORT MODELS ON THE HIGH-SPEED DOUBLE-CONE FLOWFIELD
查看参考文献32篇
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文摘
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激波与边界层之间相互作用是高超声速飞行中的常见现象,对飞行器气动性能与飞行安全至关重要.对于高焓来流,流场中通常存在复杂的物理化学现象,此时准确模拟流场中激波边界层相互作用的难度大,相关物理化学建模仍有待进一步考察和研究.本文针对最近文献中纯净空气高超声速双锥绕流实验开展数值研究,分别研究了不同热化学模型与输运模型对壁面压力与热流的影响.热力学模型包括完全气体、热力学平衡和非平衡模型,化学模型包括冻结和非平衡化学模型,输运模型包括经典的Wilke/Blottner/Eucken模型与更加复杂的Gupta/SCEBD模型,以及考虑壁面催化/非催化影响的模型.计算了6个不同算例,涵盖了低焓至高焓来流等不同工况.壁面压力与热流的数值计算结果与实验结果符合较好;对于低焓来流,计算结果主要受到分子内能分布的影响,输运模型对计算结果的影响不大;对于高焓来流,一方面计算结果受到化学反应与壁面催化的影响较大,另一方面不同输运模型对计算结果的影响也更加明显. |
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其他语种文摘
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The shock wave and boundary layer interaction is common during hypersonic flight, and it is critical for the aerodynamic performance and safety of the flight vehicle. When the enthalpy of the incoming flow is high, its numerical simulation is challenging due to many complex physics and chemistry phenomena whose modelling requires further investigation and study. Hypersonic flow around a double-cone is selected as the test case and the effects of thermochemistry and transport models on the wall pressure and heat transfer rate are studied numerically. The thermochemical models include perfect gas model, thermal non-equilibrium with frozen or non-equilibrium chemistry, and thermal equilibrium with non-equilibrium chemistry. The transport models include the widely used Wilke/Blottner/Eucken model, and the more physically complicated Gupta/SCEBD model. Moreover, the influence of wall catalysis is also considered. The six experimental test runs, covering from low to high enthalpy inflow conditions, are simulated. The computed results show that the computed wall pressure and heat flux agree with the experiments. Under the low enthalpy condition, the distribution of the molecular internal energy has a big impact on the results, and the two transport models produce similar results. Under the high enthalpy condition, the chemical reaction and wall catalysis have a significant influence. Comparison of the results with the different transport models shows much larger difference for higher freestream enthalpy. |
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来源
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力学学报
,2019,51(4):1012-1021 【核心库】
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DOI
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10.6052/0459-1879-19-022
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关键词
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激波边界层相互作用
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热化学非平衡
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输运模型
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双锥
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地址
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中国科学院力学研究所, 高温气体动力学国家重点实验室, 北京, 100190
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中国科学院大学工程科学学院, 北京, 100049
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语种
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中文 |
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文献类型
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研究性论文 |
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ISSN
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0459-1879 |
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学科
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力学 |
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基金
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中国科学院先导B项目资助
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文献收藏号
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CSCD:6556944
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参考文献 共
32
共2页
|
|
1.
Harvey J.
Shock Wave-Boundary-Layer Interactions,2011
|
CSCD被引
1
次
|
|
|
|
|
2.
Candler G V. Rate-dependent energetic processes in hypersonic flow.
Progress in Aerospace Sciences,2015,72:37-48
|
CSCD被引
2
次
|
|
|
|
|
3.
Gaitonde D. Progress in shock wave/boundary layer interactions.
Progress in Aerospace Sciences,2015,72:80-99
|
CSCD被引
48
次
|
|
|
|
|
4.
张静. 高超音速双锥绕流数值模拟的格式效应分析.
北京航空航天大学学报,2008,34(4):474-477
|
CSCD被引
4
次
|
|
|
|
|
5.
石晓峰.
激波反射干扰及其热化学非平衡效应.[博士论文],2018
|
CSCD被引
2
次
|
|
|
|
|
6.
田浩. 真实气体效应对升力体舵面局部流动分离的影响.
空气动力学学报,2015,33(3):330-337
|
CSCD被引
2
次
|
|
|
|
|
7.
童福林. 激波与转捩边界层干扰非定常特性数值分析.
力学学报,2017,49(1):93-104
|
CSCD被引
16
次
|
|
|
|
|
8.
龚安龙. 高超声速激波/边界层干扰流动数值模拟研究.
空气动力学学报,2014(6):767-771
|
CSCD被引
11
次
|
|
|
|
|
9.
唐贵明. 表面台阶引起的高超声速湍流边界层分离.
力学学报,1994,26(1):113-120
|
CSCD被引
4
次
|
|
|
|
|
10.
王保国. 高超声速双锥体绕流的数值计算与流场分析.
科技导报,2010,28(14):49-55
|
CSCD被引
1
次
|
|
|
|
|
11.
冈敦殿.
超声速平板突起物及双锥绕流实验研究.[硕士论文],2013
|
CSCD被引
1
次
|
|
|
|
|
12.
Druguet M.
Comparison of physical models in computations of high-enthalpy double-cone flows. AIAA Paper 2006-3419, 2006
|
CSCD被引
1
次
|
|
|
|
|
13.
Nompelis I. Effect of vibrational nonequilibrium on hypersonic double-cone experiments.
AIAA Journal,2003,41(11):2162-2169
|
CSCD被引
5
次
|
|
|
|
|
14.
Nompelis I.
Numerical investigation of high enthalpy chemistry on hypersonic double-cone experiments. AIAA Paper 2005-584,2005
|
CSCD被引
1
次
|
|
|
|
|
15.
Nompelis I.
US3D Predictions of double-cone and hollow cylinder-flare flows at high enthalpy. AIAA Paper 2016-3344,2016
|
CSCD被引
1
次
|
|
|
|
|
16.
Holden M S.
Measure ments of real gas effects on regions of laminar shock wave/boundary layer interaction in hypervelocity flows for‘blind’code validation studies. AIAA Paper 2013-2837,2013
|
CSCD被引
1
次
|
|
|
|
|
17.
Hao J. Numerical simulation of high-enthalpy double-cone flows.
AIAA Journal,2017,55(7):1-5
|
CSCD被引
1
次
|
|
|
|
|
18.
Kianvashrad N. The effect of thermochemistry on prediction of aerothermodynamic loading over a double cone in a laminar hypersonic flow.
AIAA Aerospace Sciences Meeting, AIAA Paper 2018-1812:2018
|
CSCD被引
1
次
|
|
|
|
|
19.
Kieweg S L.
Validation assessment of hypersonic double-cone flow simulations using uncertainty quantification, sensitivity analysis, and validation metrics. AIAA Paper 2019-2278:2019
|
CSCD被引
1
次
|
|
|
|
|
20.
Ray J.
Estimation of inflow uncertainties in laminar hypersonic double-cone experiments. AIAA Paper 2019-2279:2019
|
CSCD被引
1
次
|
|
|
|
|
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