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Experimental Study of Turbulent Boundary Layers on Groove/Smooth Flat Surfaces

Hongwei MA Qiao TIAN Hui WU

热科学学报(英文版)2005,Vol.14Issue(3):193-197,5.
热科学学报(英文版)2005,Vol.14Issue(3):193-197,5.

Experimental Study of Turbulent Boundary Layers on Groove/Smooth Flat Surfaces

Experimental Study of Turbulent Boundary Layers on Groove/Smooth Flat Surfaces

Hongwei MA 1Qiao TIAN 1Hui WU1

作者信息

  • 1. School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
  • 折叠

摘要

Abstract

This paper presents an experimental investigation of the turbulent boundary layers on both groove and smooth flat surfaces. The flow structures were shown in a water tunnel using the hydrogen-bubble flow visualization technique. The measurement results indicate that: (1) the grooves can effectively reduce accumulation of low-speed fluids, decrease the number of the low-speed streaks and depress oscillation of the streaks in the sublayer; (2) the grooves can restrain forming of the horseshoe vortices in the buffer region; (3) the grooves bate oscillation and kinking of the quasi-streamwise vortices and restrain production of the hairpin vortices and the ring vortices, reducing both frequency and intensity of the turbulence bursting; (4) the grooves directly affect the flow structures in the sublayer of the boundary layer and then modulate the flow field up to the buffer region and the logarithmic region by restraining development and interaction of the vortices.

关键词

streamwise groove/turbulent boundary layer/drag reduction mechanism/coherent structure/hydrogen-bubble flow visualization

Key words

streamwise groove/turbulent boundary layer/drag reduction mechanism/coherent structure/hydrogen-bubble flow visualization

分类

数理科学

引用本文复制引用

Hongwei MA,Qiao TIAN,Hui WU..Experimental Study of Turbulent Boundary Layers on Groove/Smooth Flat Surfaces[J].热科学学报(英文版),2005,14(3):193-197,5.

基金项目

Project funded by National Natural Science Foundation of China, Grant No.50376002. ()

热科学学报(英文版)

OAEISCI

1003-2169

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