Numerical simulation method of roughness induced transition

被引:0
作者
Li H.-Y. [1 ]
Zheng Y. [1 ]
Liu D.-X. [1 ,2 ]
机构
[1] School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing
[2] Collaborative Innovation Center for Advanced Aero-Engine, Beijing
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2016年 / 31卷 / 09期
关键词
Boundary layer; Intermittency factor; Surface roughness; Transition; Transition model;
D O I
10.13224/j.cnki.jasp.2016.09.026
中图分类号
学科分类号
摘要
For the purpose of simulating roughness induced transition, the boundary conditions of turbulent dissipation rate and eddy viscosity for rough surface were added to Langtry's γ-Reθ transition model; furthermore, equivalent sand surface roughness height was introduced to rewrite the correlation equations of the transition momentum thickness Reynolds number, making it appropriate for roughness-induced transition. Numerical simulation was made by referring to the wind tunnel data of several rough flat plate experiments and variable-pressure-gradient plate experiment, in which the results were satisfactory. Main conclusions are made as follows: surface roughness will enhance the heat transfer, increase the skin friction coefficient and shift the transition position upstream in general compared with smooth cases; effects for natural transition is significant, as surface roughness of 0.15 mm could shift the transition position upstream about 40%; while affect for separating induced transition is weaker; with the increase of surface roughness, transition position and separating bubble position are shifted backwards a little, the strength of separating bubble becomes weaker while the friction coefficient increases. © 2016, Press of Chinese Journal of Aeronautics. All right reserved.
引用
收藏
页码:2251 / 2257
页数:6
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