Review of research on low-profile vortex generators to control boundary-layer separation
By John C. H. Lin. 2002
1,006 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/f2eddcab67bc1d2ef2fd204774c79b54b585d3dc
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
- B. W. van Oudheusden
- R. Humble
- P. Blinde
- J. Wesfreid
- Jean-Luc Aider
- Jean-François Beaudoin
- Fulvio Scarano
- Bernhard Wieneke
In Computational Mechanics
- B. W. van Oudheusden
- Fulvio Scarano
- R. Humble
- P. Blinde
- J. Wesfreid
- Jean-Luc Aider
- Jean-François Beaudoin
- Bernhard Wieneke
Citations in the corpus
- Drag and lift reduction of a 3D bluff-body using active vortex generators (2010, background): “5 so that the VGs work like sub-boundary or low-profile vortex generators as defined by Lin (2002).”
- Effects of micro-ramps on a shock wave/turbulent boundary layer interaction (2009, background): “This type of VG is attractive because they typically cause less drag than conventional VGs (see [10]).”