Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations
By Iván Bermejo-Moreno, L. Campo, Johan Larsson, Julien Bodart, D. Helmer, John K. Eaton. Journal of Fluid Mechanics, 2014
151 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/07ab60b62b52382d91b332e0159788b6a452f968
How researchers see this paper
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In Aerospace Engineering
- Stefan Hickel
- Vito Pasquariello
- Nikolaus A. Adams
- M. Pino Martín
- Clarence W. Rowley
- S. Priebe
- Iván Bermejo-Moreno
- Johan Larsson
In Computational Mechanics
- Stefan Hickel
- Vito Pasquariello
- Iván Bermejo-Moreno
- Clarence W. Rowley
- Julien Bodart
- Jonathan H. Tu
- Nikolaus A. Adams
- Sergio Pirozzoli
Citations in the corpus
- Unsteady effects of strong shock-wave/boundary-layer interaction at high Reynolds number (2017, methodology): “9 impinging SWBLI at a Reynolds number of Reδ0 ≈ 38 ⋅ 10(3) and deflection angle of 12○ by means of DNS, matching experimental flow conditions of Bookey et al. (2005). Their simulation covers approximately 800 δ0/U0 and addressed low-frequency aspects of the interaction. However, a direct comparison”
- Large eddy simulation with modeled wall-stress: recent progress and future directions (2016, methodology): “Bermejo-Moreno et al. (2014) performed WMLES with an equilibrium wall-model of the interactions between oblique shock waves and turbulent boundary layers in a nearly square duct. Despite the significant pressure gradients that exist within the boundary layer in the region of interaction with the sho”
- Low-frequency dynamics in a shock-induced separated flow (2016, background): “…& Martín 2007; Grilli et al. 2012; Priebe & Martín 2012; Grilli, Hickel & Adams 2013) and of the reflected shock configuration (Pirozzoli & Grasso 2006; Priebe, Wu & Martín 2009; Touber & Sandham 2009; Hadjadj 2012; Aubard, Gloerfelt & Robinet 2013; Morgan et al. 2013; Bermejo-Moreno et al. 2014).”