Large-eddy simulation of high-Reynolds-number supersonic boundary layers using the approximate deconvolution model and a rescaling and recycling technique

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Direct numerical simulation of transonic shock/boundary layer interaction under conditions of incipient separation (2010, methodology): “In the present DNS this is achieved by exploiting a modified version of the original rescaling– recycling procedure developed by Lund, Wu & Squires (1998), and extended to the compressible case by Stolz & Adams (2003) and Xu & Martin (2004).”
Unsteady effects of strong shock-wave/boundary-layer interaction at high Reynolds number (2017, methodology): “The digital filter technique is particularly suitable for the present studies as it does not generate spurious correlations of the inflow data, a drawback exhibited by recycling–rescaling techniques (Stolz & Adams 2003).”
Turbulence in supersonic boundary layers at moderate Reynolds number (2011, methodology): “Therefore, the overwhelming majority of the computational algorithms designed for LES and DNS of compressible flows rely on some form of upwinding or explicit filtering (and dealiasing in spectral simulations) for numerical stabilization, and most often incorporate some form of shock-capturing, whic”
Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction (2006, methodology): “This is accomplished by the rescaling and recycling technique of Lund, Wu & Squires (1998), formulated for compressible flow by Stolz & Adams (2003).”