Direct numerical simulation of a separated turbulent boundary layer

By Martin Skote, Dan S. Henningson. Journal of Fluid Mechanics, 2002

287 citations recorded by the source corpus.

Subfields: Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/3ff899a6c504f89f65b744379c4b49b5dbcc820c

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Computational Mechanics

In Environmental Engineering

Citations in the corpus

Large-eddy simulation of boundary-layer separation and transition at a change of surface curvature (2001, methodology): “DNS of a separated turbulent boundary layer on a flat plate in an adverse pressure gradient has been carried out recently by Na & Moin (1998).”
SIMSON : A Pseudo-Spectral Solver for Incompressible Boundary Layer Flows (2007, background): “Direct numerical simulation of a separated turbulent boundary layer (Skote & Henningson, 2002) 14.”
History effects and near equilibrium in adverse-pressure-gradient turbulent boundary layers (2017, methodology): “Moreover, power-law distributions of U∞ were also considered in the numerical studies by Skote, Henningson & Henkes (1998), Lee & Sung (2009) and Lee (2017), focused on attached APG TBLs, and by Skote & Henningson (2002) where the aim was to characterize separated APG TBLs.”
Highly resolved large-eddy simulation of separated flow in a channel with streamwise periodic constrictions (2005, background): “In fact, the concept of a single line of separation or reattachment, while pertinent to the average flow, is not meaningful for the instantaneous flow separating from a smooth wall (Na & Moin 1998).”
Three-dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction (2009, result): “The present results are also reminiscent of the DNS of incompressible separated flows by Na & Moin (1998) and Chong et al. (1998), who showed that vortical structures and the vorticity layer are lifted away from the wall in the first part of the separation process.”
Numerical investigation of the tone noise mechanism over laminar airfoils (2007, background): “…has the same features as those reported by Alam & Sandham (2000) in the two-dimensional simulation of a short laminar bubble which exhibits self-sustained vortex shedding, and is significantly different from that of the numerical simulation of a separated turbulent boundary layer (Na & Moin 1998).”
Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685 (2000, background): “The profiles after reattachment are similar to those observed by Na & Moin (1998) for a flat-plate boundary layer with separation.”
Direct numerical simulation of transonic shock/boundary layer interaction under conditions of incipient separation (2010, background): “As observed by Pirozzoli & Grasso (2006) in the case of an impinging shock/boundary layer interaction at supersonic Mach number, and by Na & Moin (1998a) for a low-speed turbulent boundary layer under APG, the instantaneous pressure field highlights the formation of pressure minima associated with…”