Bulletin of the American Physical Society
71st Annual Meeting of the APS Division of Fluid Dynamics
Volume 63, Number 13
Sunday–Tuesday, November 18–20, 2018; Atlanta, Georgia
Session A20: Turbulent Boundary Layers I
8:00 AM–9:57 AM,
Sunday, November 18, 2018
Georgia World Congress Center
Room: B308
Chair: Corey Markfort, University of Iowa
Abstract ID: BAPS.2018.DFD.A20.9
Abstract: A20.00009 : Investigation of the factors contributing to skin friction coefficient in a self-similar adverse pressure gradient (APG) turbulent boundary layer (TBL) flow using direct numerical simulation (DNS)*
9:44 AM–9:57 AM
Presenter:
Shevarjun Senthil
(Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechanical and Aerospace Engineering, Monash University, Melbourne 3800, Australia)
Authors:
Shevarjun Senthil
(Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechanical and Aerospace Engineering, Monash University, Melbourne 3800, Australia)
Callum Atkinson
(Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechanical and Aerospace Engineering, Monash University, Melbourne 3800, Australia)
Vassili Kitsios
(CSIRO Oceans and Atmosphere, Castray Esplanade, Battery Point, Tasmania 7004, Australia, Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechani)
Atsushi Sekimoto
(Department of Materials Engineering Science, Osaka University, Osaka 560-8531, Japan, Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechanical)
Julio Soria
(Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechanical and Aerospace Engineering, Monash University, Melbourne 3800, Australia)
DNS is performed to solve the incompressible Navier-Stokes equation for pressure and velocity in a self-similar APG-TBL.2 We study the contributions to the skin friction coefficient (Cf) from turbulent fluctuations, viscous effects and pressure gradient. Cf is calculated based on the formulation given by Renard and Deck for boundary layer (BL) flows.3 The non-dimensional pressure gradient (β) is defined as β = δ1 Pe,x / τw where δ1 is the displacement thickness, Pe,x is the far-field pressure gradient and τw is the mean wall shear stress. The Cf decomposition is studied for three different BL flows with β = 0, 1 and 39. With increasing β, Cf approaches zero and the flow becomes more like a free shear layer. It is found that the contribution from viscous effects reduces as β changes from 0 to 39. The Reynolds stress remains the dominant contributor for all β and its contribution to Cf has a peak at y = δ1 for β = 39 where y is the wall normal direction.
*1This work was supported by the Australian Research Council, the Pawsey Supercomputing Centre and the Australian National Computational Infrastructure through a NCMAS grant. 2Kitsios V. et al. J. Fluid Mech, 392–419, 829, 2017. 3Renard N. and Deck S. J. Fluid Mech, 339–367, 790, 2016.
To cite this abstract, use the following reference: http://meetings.aps.org/link/BAPS.2018.DFD.A20.9
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