Analysis of the Contribution of Large Scale Motions to the Skin Friction of a Zero-Pressure-Gradient Turbulent Boundary Layer Using the Renard-Deck Decomposition

Authors

  • Bihai Sun Laboratory for Turbulence Research in Aerospace & Combustion (LTRAC) Department of Mechanical and Aerospace Engineering, Monash University, Australia
  • Muhammad Shehzad Laboratory for Turbulence Research in Aerospace & Combustion (LTRAC) Department of Mechanical and Aerospace Engineering, Monash University, Australia
  • Daniel Jovic Laboratory for Turbulence Research in Aerospace & Combustion (LTRAC) Department of Mechanical and Aerospace Engineering, Monash University, Australia
  • Christophe Cuvier Université Lille Nord de France, LMFL - Laboratoire de Mécanique des Fluides de Lille
  • Christian Willert Institute of Propulsion Technology, German Aerospace Center (DLR), Cologne, Germany
  • Yasar Ostovan Université Lille Nord de France, LMFL - Laboratoire de Mécanique des Fluides de Lille
  • Jean-Marc Foucaut Universite Lille Nord de France, Laboratoire de Mecanique des fluides de Lille Kampe de Feriet, Lille, France
  • Callum Atkinson Laboratory for Turbulence Research in Aerospace & Combustion (LTRAC) Department of Mechanical and Aerospace Engineering, Monash University, Australia
  • Julio Soria Laboratory for Turbulence Research in Aerospace & Combustion (LTRAC) Department of Mechanical and Aerospace Engineering, Monash University, Australia

DOI:

https://doi.org/10.18409/ispiv.v1i1.173

Abstract

Coherent flow structures in turbulent boundary layers have been an active field of research for many decades, as they might be the key to reveal the mechanics of turbulence production and transport in turbulent shear flows. Renard and Deck (2016) proposed a theoretical decomposition for the mean skin-friction coefficient based on the mean kinetic energy budget in the streamwise direction. This decomposition, referred to as the Renard-Deck (RD) decomposition, decomposes the mean skin friction generation into three physical mechanisms in an absolute reference frame, namely, direct viscous dissipation, turbulent kinetic energy production, and spatial growth. In this study, the large scale motions (LSMs) are extracted using a proper orthogonal decomposition (POD) of the velocity field based on high-spatial-resolution two-dimensional – two-component particle image velocimetry (HSR 2C-2D PIV) of a zero-pressure-gradient turbulent boundary layer (ZPG-TBL), and their effect on the skin friction via RD decomposition.

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Published

2021-08-01

Issue

Section

Boundary Layers