Direct numerical simulations of forced and unforced separation bubbles on an airfoil at incidence
By L. E. Jones, Richard D. Sandberg, Neil D. Sandham. Journal of Fluid Mechanics, 2008
398 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/aad18098831fbdb187d5da3060e609143de091db
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
- Tamer A. Zaki
- L. E. Jones
- Dan S. Henningson
- Richard D. Sandberg
- Olaf Marxen
- R. Radespiel
- P. Durbin
- Christian J. Kähler
In Computational Mechanics
- Tamer A. Zaki
- L. E. Jones
- Dan S. Henningson
- Olaf Marxen
- Richard D. Sandberg
- Wolfgang Rodi
- P. Durbin
- Christian J. Kähler
Citations in the corpus
- Stability and receptivity characteristics of a laminar separation bubble on an aerofoil (2010, methodology): “In Jones et al. (2008) no regions of absolute instability were observed for the time-averaged aerofoil flow with separation bubble, as determined via linear stability analysis.”
- Acoustic and hydrodynamic analysis of the flow around an aerofoil with trailing-edge serrations (2012, background): “It should be noted that the grid-resolution is specified to yield y+ = 1 at the wall, and ten grid-points below y+ = 10, at the worst-case location of maximum skin friction for the equivalent case without splitter plate (approximately x = 0.7: Jones et al. 2008).”
- The effect of small-amplitude convective disturbances on the size and bursting of a laminar separation bubble (2011, methodology): “However, it cannot be ruled out that the occurrence of small-scale three-dimensional structures is aided by an absolute primary (global) instability (Theofilis 2003) or, more likely, a secondary absolute instability (Maucher, Rist & Wagner 2000b; Marxen, Rist & Wagner 2004; Jones et al. 2008).”
- Dynamics of laminar separation bubbles at low-Reynolds-number aerofoils (2009, methodology): “From other investigations (Marxen et al. 2004; Jones et al. 2008) it is well known that a forcing of the TS waves affects the separation bubble.”
- Direct numerical simulations of transition in a compressor cascade: the influence of free-stream turbulence (2010, background): “This interaction is similar to that reported by Jones et al. (2008).”