华南理工大学学报(自然科学版) ›› 2021, Vol. 49 ›› Issue (6): 9-18.doi: 10.12141/j.issn.1000-565X.200454

所属专题: 2021年机械工程

• 机械工程 • 上一篇    下一篇

平板表面边界层流态结构的数值模拟

和生泰 兰巍 胡兴军   

  1. 吉林大学 汽车仿真与控制国家重点实验室,吉林 长春 130022
  • 收稿日期:2020-08-03 修回日期:2020-12-30 出版日期:2021-06-25 发布日期:2021-06-01
  • 通信作者: 胡兴军(1976-),男,教授,博士生导师,主要从事汽车空气动力学研究。 E-mail:hxj@jlu.edu.cn
  • 作者简介:和生泰(1994-),男,博士,主要从事汽车空气动力学研究。E-mail:17390955857@163.com
  • 基金资助:
    国家自然科学基金资助项目(51875238)

Numerical Simulation of Flow Pattern Structure in Boundary Layer on Flat Plate Surfaces

HE Shengtai LAN Wei HU Xingjun   

  1. State Key Laboratory of Automotive Simulation and Control, Jilin University, Changchun 130022, Jilin , China
  • Received:2020-08-03 Revised:2020-12-30 Online:2021-06-25 Published:2021-06-01
  • Contact: 胡兴军(1976-),男,教授,博士生导师,主要从事汽车空气动力学研究。 E-mail:hxj@jlu.edu.cn
  • About author:和生泰(1994-),男,博士,主要从事汽车空气动力学研究。E-mail:17390955857@163.com
  • Supported by:
    Supported by the National Natural Science Foundation of China(51875238)

摘要: 采用γ-Reθt转捩模型对平板表面边界层进行了数值模拟,研究了边界层在法向和流向上的发展变化以及壁面粗糙度、来流风速、湍流度、压力梯度等因素对边界层发展的影响。研究结果表明:在转捩区间内壁面摩擦系数以及离壁面一定高度处的总压会发生突变,边界层厚度沿流向不断增厚但其增长率不断下降;层流边界层中黏应力占主导,湍流边界层中应力变化依次为黏应力占主导、黏应力不断下降而雷诺应力不断上升、雷诺应力占主导,分别对应层流底层、过渡层、对数层与外层;转捩过程中黏应力在壁面处达到的峰值不断增大而其衰减变得更快,雷诺应力的峰值不断增大但达到峰值时对应的法向高度不断降低;粗糙度的增大使湍流边界层黏性底层消失,对数律层下移;湍流度和风速的增大使转捩提前,转捩区间缩短,同时降低了湍流边界层增长率;压力梯度则对湍流边界层增长率影响很大,逆压梯度易使边界层快速增厚。

关键词: 平板边界层, 转捩, 雷诺应力, 黏应力

Abstract: The γ-Reθt  transition model was used to numerically simulate the boundary layer on the surface of the plate. The development of the boundary layer in the normal and the flow direction, as well as the effect of factors such as wall roughness,incoming wind speed,turbulence intensity, and pressure gradient on the boundary layer were studied. The study show that, in the transition interval, skin-friction coefficient and the total pressure at a certain height from the wall undergo abrupt changes; in the flow direction, the boundary layer continues to thicken but its growth rate continues to decline; in the laminar boundary layer, the viscous stress is dominant, but in the turbulent boundary layer, the sub-layer is firstly dominated by viscous stress, then the viscous stress decreases rapidly and the Reynolds stress increases rapidly, finally Reynolds stress is dominant in the log-law region. During the transition process, the maximum value of the viscous stress near the wall continues to increase but its attenuation becomes faster. The maximum value of Reynolds stress continues to increase but the normal height corresponding to the maximum value continues to decrease. The increase in roughness makes the viscous sub-layer of the turbulent boundary layer disappears and the log-law layer moves down. The increase of turbulence intensity and wind speed advances the transition, shortens the transition interval, and reduces the growth rate of the turbulent boundary layer. The pressure gradient has a great influence on the growth rate of the turbulent boundary layer, and the adverse pressure gradient thickens the boundary layer quickly.

Key words: flat boundary layer, transition, Reynolds stress, viscous stress

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