Coherent structures in direct numerical simulation of turbulent boundary layers at Mach 3

By M. Ringuette, Minwei Wu, M. Pino Martín. Journal of Fluid Mechanics, 2007

143 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/1117a19740a27808f9c975427195a34ef0432346

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In Computational Mechanics

Citations in the corpus

Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number (2011, unknown): “and it has been used by several researchers to infer the existence of coherent structures (Brown & Thomas 1977; Ringuette et al. 2008; O’Farrell & Martı́n 2009).”
Turbulence in supersonic boundary layers at moderate Reynolds number (2011, background): “Evidence for clustering of symmetric and asymmetric hairpinlike vortices above low-speed superstructures in supersonic boundary layers was also provided from DNS data at lower Re (Ringuette et al. 2008), and from experiments (Elsinga et al. 2010).”
Three-dimensional vortex organization in a high-Reynolds-number supersonic turbulent boundary layer (2010, result): “4δ, which is consistent with earlier studies (Spina et al. 1991; Tomkins & Adrian 2003; Ganapathisubramani et al. 2006; Ringuette et al. 2008), and the spanwise spacing between low-speed zones is typically between 0.”
Characterization of coherent vortical structures in a supersonic turbulent boundary layer (2008, background): “In order to alleviate such deficiency, the geometrical properties of vortical structures are determined by subtracting out the mean shear, as was also done by Robinson (1991b). We point out that, in principle, mean shear and turbulent fluctuations cannot be decoupled.”
Coherent Structures and the Dissimilarity of Turbulent Transport of Momentum and Scalars in the Unstable Atmospheric Surface Layer (2011, background): “Kline et al. 1967; Head and Bandyopadhyay 1981; Kim and Adrian 1999; Monty et al. 2007; Ringuette et al. 2008; Marusic et al. 2010a).”
Experimental measurement of large-scale three-dimensional structures in a turbulent boundary layer. Part 2. Long structures (2011, methodology): “2), and in some cases a few data points from Spalart (1988) at Reθ =1410 have also been included. It should be noted that although the Reynolds number of the Spalart (1988) data is different from the case presented here, the Reynolds stresses in the outer part of the boundary layer are fairly insens”
Three-dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction (2009, methodology): “…in compressible boundary layers by many other authors, such as Samimy et al. (1994), Ganapathisubramani et al. (2006), Elsinga et al. (2007), and Ringuette et al. (2008) for instance, as well as in incompressible boundary layers by Kim & Adrian (1999), Hutchins & Marusic (2007), Tomkins &…”