Simulations of bypass transition

By R. G. Jacobs, P. Durbin. Journal of Fluid Mechanics, 2001

516 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Civil and Structural Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/fcb9dc0fe37ff370e4d2b032cfa893fba9113074

How researchers see this paper

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

In Aerospace Engineering

In Civil and Structural Engineering

In Computational Mechanics

Citations in the corpus

Leading-edge effects in bypass transition (2007, methodology): “While the backward jet mechanism of Jacobs & Durbin (2001) seems to be the same as the streak sinuous mode, they do not report the varicose mode.”
Direct numerical simulation of turbulence in a nominally zero-pressure-gradient flat-plate boundary layer (2009, methodology): “Jacobs & Durbin (2001) computed a ZPGFPBL for a momentum thickness Reynolds number range of 120 Reθ 1000 on 70 million grid points.”
Nonmodal Stability Theory (2007, background): “Experimental observations (e.g., Alfredsson & Matsubara 2000), as well as direct numerical simulations (e.g., Berlin & Henningson 1999, Jacobs & Durbin 2001), of many wall-bounded shear flows, however, provide abundant evidence for the streamwise-vortices-streaks scenario under natural conditions.”
Transition of streamwise streaks in zero-pressure-gradient boundary layers (2002, background): “Jacobs & Durbin (2001) conjecture that streaks become a receptivity site for smaller-scale free-stream turbulence which initiates an instability near the top of the boundary layer.”
Direct numerical simulations of transition in a compressor cascade: the influence of free-stream turbulence (2010, background): “Jacobs & Durbin (2000) suggested that breakdown in bypass transition commences near the top of the boundary layer, when the negative u′t perturbations are exposed to high-frequency forcing in the free stream.”
Transition in boundary layers subject to free-stream turbulence (2004, methodology): “Implementing the methodology first proposed by Grosch & Salwen (1978), these authors constructed a turbulent inflow by expanding the free-stream turbulence as a sum of spanwise and temporal Fourier modes, multiplied by wall-normal Orr–Sommerfeld modes.”
Mode interaction and the bypass route to transition (2005, methodology): “Hence, disturbances near the leading edge decay (Jacobs & Durbin 2000), and the coupling that leads to boundary layer jets and transition is local, in the downstream region (Leib et al. 1999).”
Transition induced by free-stream turbulence (2005, background): “There have also recently been some direct numerical simulations of the FST transition process (see Jacobs & Durbin 2001; Brandt, Schlatter & Henningson 2004).”
Modelling Bypass Transition with Low-Reynolds-Number Nonlinear Eddy-Viscosity Closure (2004, background): “The main features of the simulated flow are conveyed by Figures 13 and 14 which show, respectively, the structure of the flow and the stream-wise distribution of the shape factor, which are in good agreement with previous studies [ 10 , 29].”