Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators
By G. Godard, Michel Stanislas. 2006
385 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/4bab01aff8ddbb099022293788044e190fcdf6b4
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Drag and lift reduction of a 3D bluff-body using active vortex generators (2010, background): “4.2 Influence of the spacing between the vortex generators It is well known from previous studies (Godard and Stanislas 2006; Lin et al. 2002) that the spacing between the 3D perturbations induced by vortex generators has a strong influence on their efficiency on the forced flow.”
- Numerical study of passive and active flow separation control over a NACA0012 airfoil (2008, neutral): “[12] conducted an experimental study to optimize the standard passive vane-type vortex generators over of bump in a boundary layer wind tunnel, which mimics the adverse pressure gradient on the suction side of an airfoil at the verge of separation.”