首页|高焓湍流边界层直接数值模拟与湍流模型改进研究

高焓湍流边界层直接数值模拟与湍流模型改进研究

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随着高超声速飞行器速度的进一步提高,高温化学反应与湍流耦合问题将愈加突出.分别对高焓和低焓流动条件下的平板湍流边界层进行了直接数值模拟(Direct Numerical Simulation,DNS),并将湍流平均量、湍动能生成项、湍流摩擦阻力系数等物理量与SST湍流模型进行了对比分析.初步研究表明,在低焓来流条件下,SST模型与DNS的计算结果较为吻合,而在高焓条件下,受到化学反应的影响,SST湍流模型预测的湍动能、湍流黏性系数、湍流摩阻系数均高于DNS计算结果.因此,修正了针对高焓流动条件下的SST湍流模型,在k方程湍动能生成项中加入温度限制器,改进后结果与DNS计算结果值吻合较好.
Direct numerical simulation and modeling of turbulent boundary layer in high-enthalpy flows
With the further increase of hypersonic vehicle velocity,the coupling problem of high temperature chemical reaction and turbulence will become more and more prominent.The direct numerical simulation(DNS)of the turbulent boundary layer under the conditions of high-enthalpy flow and low-enthalpy flow is carried out respectively,and the physical quantities such as turbulent mean quantity,turbulent kinetic energy generation term and turbulent friction resistance coefficient are compared with the SST turbulence model.The preliminary results show that under the condition of low-enthalpy flow,the turbulent kinetic energy,turbulent viscosity coefficient and turbulent friction coefficient predicted by SST turbulence model are all higher than those calculated by DNS due to the influence of chemical reaction under high-enthalpy condition.Therefore,the SST turbulence model under high-enthalpy flow conditions is modified,and a temperature limiter is added to the turbulent kinetic energy generation term of k equation.The improved results are in good agreement with the calculated values of DNS.

high-enthalpy flowturbulent boundary layerchemical non-equilibriumdirect numeri-cal simulationturbulence model

左政玄、赵瑞、樊宇翔

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北京理工大学,北京 100081

北京理工大学重庆创新中心,重庆 401135

高焓流动 湍流边界层 化学非平衡 直接数值模拟 湍流模型

2024

空天技术
北京海鹰科技情报研究所(中国航天科工集团第三研究院310研究所)

空天技术

CSTPCD北大核心
影响因子:0.402
ISSN:2097-0714
年,卷(期):2024.(2)
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