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带有压力梯度的平板边界层转捩数值模拟
引用本文:董平,黄洪雁,冯国泰.带有压力梯度的平板边界层转捩数值模拟[J].航空动力学报,2007,22(11):1909-1914.
作者姓名:董平  黄洪雁  冯国泰
作者单位:哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001
基金项目:国家自然科学基金 , 国家自然科学基金
摘    要:对零压力梯度和带有压力梯度的平板边界层转捩实验T3A,T3C1和T3C2进行了数值模拟,计算结果与实验值吻合的较好,并得出以下的结论:压力梯度的存在对转捩起始的位置有较大的影响;M-L转捩模型能比较准确地预测转捩的发生和发展过程,但M-L一方程转捩模型因为要根据经验选取转捩起始动量厚度雷诺数,所以在通用性上相对M-L二方程转捩模型要弱;使用M-L转捩模型计算过程中,根据湍流的性质选取进口粘性比有助于正确地预测转捩的发展过程.

关 键 词:航空、航天推进系统  压力梯度  平板边界层转捩  转捩模型  数值模拟  压力梯度  平板  边界层转捩  数值模拟  pressure  gradient  boundary  layer  transition  simulation  进口  性质  湍流  计算过程  使用  通用性  雷诺数  动量厚度  选取  方程  发展过程  发生  预测
收稿时间:2006/11/6 0:00:00
修稿时间:2007/1/11 0:00:00

Numerical simulation of boundary layer transition under pressure gradient
DONG Ping,HUANG Hong-yan and FENG Guo-tai.Numerical simulation of boundary layer transition under pressure gradient[J].Journal of Aerospace Power,2007,22(11):1909-1914.
Authors:DONG Ping  HUANG Hong-yan and FENG Guo-tai
Institution:School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China;School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China;School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Abstract:Numerical simulation was performed for the flat plate boundary layer transition test at zero and non-zero pressure gradients,T3A,T3C1 and T3C2.The results have been validated through the experimental data,showing that the pressure gradient could have great influence upon the starting position of transition process;ML transition model could predict accurately the transition and development process.However,the applicability of M-L one-equation transition model is limited as compared with M-L two-equation transition model,since it depends on how to correctly choose the transition onset momentum thickness Reynolds number by experiences.During calculation with M-L transition model,selecting the import viscosity based on the nature of vortex assists in predicting the transition process.
Keywords:aerospace propulsion system  pressure gradient  flat plate boundary layer transition  transition model  numerical simulation
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