Large-Eddy Simulation of a Supersonic Boundary Layer Using an Unstructured Grid

By G. Urbin, Doyle D. Knight. 2001

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Flow physics and RANS modelling of oblique shock/turbulent boundary layer interaction (2013, methodology): “RR + DR represents an improvement of the traditional recycling/rescaling (RR) method for compressible boundary layers developed by Urbin & Knight (2001) in which the recycled profile is first reflected about a dynamically selected spanwise location.”
Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity (2015, methodology): “A recycling/rescaling method [22] is used to treat the turbulent inflow condition, which is considered to be a promising way to prescribe time-dependent turbulent inflow conditions for LES or hybrid RANS/LES of spatially developing turbulent flows [27–30].”
Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations (2014, background): “However, one of the main advantages over existing alternatives such as rescaling/recycling (Lund, Wu & Squires 1998; Urbin & Knight 2001; Morgan et al. 2011) is that no low-frequency forcing is added at the inflow (Touber & Sandham 2009b, 2011) that could otherwise interfere with any intrinsic…”