The amplification of large-scale motion in a supersonic concave turbulent boundary layer and its impact on the mean and statistical properties
The amplification of large-scale motion in a supersonic concave turbulent boundary layer and its impact on the mean and statistical properties
Direct numerical simulation is conducted to uncover the response of a supersonic turbulent boundary layer to streamwise concave curvature and the related physical mechanisms at a Mach number of 2.95. Streamwise variations of mean flow properties, turbulence statistics and turbulent structures are analysed. A method to define the boundary layer thickness based on the principal strain rate is proposed, which is applicable for boundary layers subjected to wall-normal pressure and velocity gradients. While the wall friction grows with the wall turning, the friction velocity decreases. A logarithmic region with constant slope exists in the concave boundary layer. However, with smaller slope, it is located lower than that of the flat boundary layer. Streamwise varying trends of the velocity and the principal strain rate within different wall-normal regions are different. The turbulence level is promoted by the concave curvature. Due to the increased turbulence generation in the outer layer, secondary bumps are noted in the profiles of streamwise and spanwise turbulence intensity. Peak positions in profiles of wall-normal turbulence intensity and Reynolds shear stress are pushed outward because of the same reason. Attributed to the Görtler instability, the streamwise extended vortices within the hairpin packets are intensified and more vortices are generated. Through accumulations of these vortices with a similar sense of rotation, large-scale streamwise roll cells are formed. Originated from the very large-scale motions and by promoting the ejection, sweep and spanwise events, the formation of large-scale streamwise roll cells is the physical cause of the alterations of the mean properties and turbulence statistics. The roll cells further give rise to the vortex generation. The large number of hairpin vortices formed in the near-wall region lead to the improved wall-normal correlation of turbulence in the concave boundary layer.
454-493
Wang, Qian-Cheng
3151451c-fa02-45cf-bc3b-7bcdc4ca2e0c
Wang, Zhen-Guo
ef84d30a-bca2-4dc2-982b-00356323b76e
Sun, Ming-Bo
552a7e25-e527-4c6f-b1dc-f733090bb63b
Yang, Rui
c75e3daa-35bb-45c4-b9b2-781af99d83bb
Zhao, Yu-Xin
4733ed03-6f1a-4739-ae79-4b18f23e99c3
Hu, Zhiwei
dd985844-1e6b-44ba-9e1d-fa57c6c88d65
Wang, Qian-Cheng
3151451c-fa02-45cf-bc3b-7bcdc4ca2e0c
Wang, Zhen-Guo
ef84d30a-bca2-4dc2-982b-00356323b76e
Sun, Ming-Bo
552a7e25-e527-4c6f-b1dc-f733090bb63b
Yang, Rui
c75e3daa-35bb-45c4-b9b2-781af99d83bb
Zhao, Yu-Xin
4733ed03-6f1a-4739-ae79-4b18f23e99c3
Hu, Zhiwei
dd985844-1e6b-44ba-9e1d-fa57c6c88d65
Wang, Qian-Cheng, Wang, Zhen-Guo, Sun, Ming-Bo, Yang, Rui, Zhao, Yu-Xin and Hu, Zhiwei
(2019)
The amplification of large-scale motion in a supersonic concave turbulent boundary layer and its impact on the mean and statistical properties.
Journal of Fluid Mechanics, 863, .
(doi:10.1017/jfm.2018.1004).
Abstract
Direct numerical simulation is conducted to uncover the response of a supersonic turbulent boundary layer to streamwise concave curvature and the related physical mechanisms at a Mach number of 2.95. Streamwise variations of mean flow properties, turbulence statistics and turbulent structures are analysed. A method to define the boundary layer thickness based on the principal strain rate is proposed, which is applicable for boundary layers subjected to wall-normal pressure and velocity gradients. While the wall friction grows with the wall turning, the friction velocity decreases. A logarithmic region with constant slope exists in the concave boundary layer. However, with smaller slope, it is located lower than that of the flat boundary layer. Streamwise varying trends of the velocity and the principal strain rate within different wall-normal regions are different. The turbulence level is promoted by the concave curvature. Due to the increased turbulence generation in the outer layer, secondary bumps are noted in the profiles of streamwise and spanwise turbulence intensity. Peak positions in profiles of wall-normal turbulence intensity and Reynolds shear stress are pushed outward because of the same reason. Attributed to the Görtler instability, the streamwise extended vortices within the hairpin packets are intensified and more vortices are generated. Through accumulations of these vortices with a similar sense of rotation, large-scale streamwise roll cells are formed. Originated from the very large-scale motions and by promoting the ejection, sweep and spanwise events, the formation of large-scale streamwise roll cells is the physical cause of the alterations of the mean properties and turbulence statistics. The roll cells further give rise to the vortex generation. The large number of hairpin vortices formed in the near-wall region lead to the improved wall-normal correlation of turbulence in the concave boundary layer.
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The amplification of large-scale motion in a supersonic submitted
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Accepted/In Press date: 12 December 2018
e-pub ahead of print date: 29 January 2019
Identifiers
Local EPrints ID: 428440
URI: http://eprints.soton.ac.uk/id/eprint/428440
ISSN: 0022-1120
PURE UUID: d9b0ed3d-b09b-4dde-86c4-125b52290aac
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Date deposited: 27 Feb 2019 17:30
Last modified: 16 Mar 2024 07:38
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Author:
Qian-Cheng Wang
Author:
Zhen-Guo Wang
Author:
Ming-Bo Sun
Author:
Rui Yang
Author:
Yu-Xin Zhao
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