Assessment of inflow boundary conditions for compressible turbulent boundary layers

By Sheng Xu, M. Pino Martín. 2004

207 citations recorded by the source corpus.

Subfields: Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/ba2d3cd5b360797d32d8a3c155b56983c2f9dbf0

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In Computational Mechanics

In Environmental Engineering

Citations in the corpus

Numerical Methods for High-Speed Flows (2011, methodology): “A frequently used technique is the rescaling-recycling procedure developed by Lund et al. (1998), and extended to the compressible case by Sagaut et al. (2004) and Xu & Mart́ın (2004).”
Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number (2011, unknown): “Using periodic boundary conditions, the change in (δ∗, uτ , Cf ) across the fields for ensemble averaging is less than 5 % and the flow can be viewed as a good approximation of a boundary layer at a static station (see Xu & Martı́n 2004).”
Direct numerical simulation of hypersonic turbulent boundary layers. Part 1. Initialization and comparison with experiments (2007, methodology): “A flow that satisfies these conditions evolves slowly and can be viewed as a good approximation of a static station of a boundary layer (Xu & Martin 2003, 2004).”
Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature (2010, background): “During this time period, the change in (δ, uτ , Cf ) is less than 5 % and thus the flow is a good approximation to a static station of a boundary layer (see Xu & Martin 2004).”
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).”
A bandwidth-optimized WENO scheme for the effective direct numerical simulation of compressible turbulence (2006, methodology): “The initial conditions are those of Marti´n [29] and we use rescaling boundary conditions [ 30 ] to provide the inflow.”
Turbulence in supersonic boundary layers at moderate Reynolds number (2011, methodology): “…on the idea of following the entire process of boundary layer transition starting from laminar inflow conditions into the fully developed region (Pirozzoli, Grasso & Gatski 2004), or on the extension of Lund’s recycling–rescaling technique (Stolz & Adams 2003; Xu & Martin 2004; Lagha et al. 2011).”