Abstract
A flow-control method is applied to enhance the efficiency and flow homogeneity of three-dimensional diffusers used in open-jet wind tunnels. Suitably shaped grooves are introduced in the diffuser diverging walls. The grooves promote the relaxation of the non-slip condition along the streamlines bounding the small recirculation regions forming passively inside the grooves. That reduces momentum losses and results in a downstream boundary layer with higher momentum, which is more separation-resistant.
In this study, circular and square-section diffusers with different degrees of flow separation were examined. The grooves significantly enhanced performance in circular diffusers by reducing the extent of separation and promoting an axisymmetric and spatially uniform flow. However, negligible benefits were observed for square-section diffusers. In these cases, since flow separation originates from one of the four inclined edges of the diffuser, placing grooves along the diverging walls does not effectively reduce the separation extent. Nonetheless, the grooves become effective again in diffusers with rectangular cross sections of high aspect ratio.
Conference/Journal: Physics of Fluids 36(10), 105164 (October 2024)
DOI/Source: https://pubs.aip.org/aip/pof/article-abstract/36/10/105164
Keywords: CFD, Computational fluid dynamics, Aerodynamics, Flow control, Boundary layer flow, Turbulent flows