Abstract
In aerodynamics, the laminar or turbulent regime of a boundary layer has a strong influence on friction or heat transfer. In practical applications, it is sometimes necessary to trip the transition to turbulent, and a common way is by use of a roughness element (e.g. a step) on the wall. The present paper is concerned with the numerical implementation of such a trip in large-eddy simulations. The study is carried out on a flat-plate boundary layer configuration, with Reynolds number Rex=1.3×106. First, this work brings the opportunity to introduce a practical methodology to assess convergence in large-eddy simulations. Second, concerning the trip implementation, a volume source term is proposed and is shown to yield a smoother and faster transition than a grid step. Moreover, it is easier to implement and more adaptable. Finally, two subgrid-scale models are tested: the WALE model of Nicoud and Ducros (Flow Turbul. Combust., vol. 62, 1999) and the shear-improved Smagorinsky model of Lévêque et al. (J. Fluid Mech., vol. 570, 2007). Both models allow transition, but the former appears to yield a faster transition and a better prediction of friction in the turbulent regime.
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Abbreviations
- α :
-
power-law factor
- β :
-
minus power-law exponent
- χ :
-
numerical convergence monitor
- Δx +, Δy +, Δz + :
-
cell-dimensions at wall, in wall units (streamwise, wall-normal, spanwise)
- δ :
-
boundary-layer thickness
- δ̣✩ :
-
displacement thickness
- ɛ 4 :
-
artificial viscosity coefficient
- µ:
-
dynamic viscosity
- θ :
-
momentum thickness
- ρ :
-
density
- a :
-
contravariant vector
- C D :
-
drag coefficient
- C f :
-
friction coefficient
- c :
-
speed of sound
- h:
-
cell volume
- LES :
-
large-eddy simulation
- L x , L y , L z :
-
minimum domain dimensions
- l x , l y :
-
step dimensions (length and height)
- RANS :
-
Reynolds-averaged Navier-Stokes
- Re x :
-
Reynolds number (based on axial distance)
- T:
-
static temperature
- t:
-
time
- t+ :
-
normalized time
- U:
-
mean streamwise velocity
- u :
-
velocity vector
- u, v, w:
-
velocity components (eq. u x , u y , u z )
- u w :
-
friction velocity
- x, y, z:
-
coordinates (streamwise, wall-normal and spanwise)
- x trip :
-
trip abscissa
- ∞:
-
infinity index: inflow characteristics
- —:
-
overline: mean
- ′:
-
prime: standard deviation
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Boudet, J., Monier, J.F. & Gao, F. Implementation of a roughness element to trip transition in large-eddy simulation. J. Therm. Sci. 24, 30–36 (2015). https://doi.org/10.1007/s11630-015-0752-8
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DOI: https://doi.org/10.1007/s11630-015-0752-8