Drag and lift reduction of a 3D bluff-body using active vortex generators

In this study, a passive flow control experiment on a 3D bluff-body using vortex generators (VGs) is presented. The bluff-body is a modified Ahmed body (Ahmed in J Fluids Eng 105:429–434 1983) with a curved rear part, instead of a slanted one, so that the location of the flow separation is no longer forced by the geometry. The influence of a line of non-conventional trapezoïdal VGs on the aerodynamic forces (drag and lift) induced on the bluff-body is investigated. The high sensitivity to many geometric (angle between the trapezoïdal element and the wall, spanwise spacing between the VGs, longitudinal location on the curved surface) and physical (freestream velocity) parameters is clearly demonstrated. The maximum drag reduction is −12%, while the maximum global lift reduction can reach more than −60%, with a strong dependency on the freestream velocity. For some configurations, the lift on the rear axle of the model can be inverted (−104%). It is also shown that the VGs are still efficient even downstream of the natural separation line. Finally, a dynamic parameter is chosen and a new set-up with motorized vortex generators is proposed. Thanks to this active device. The optimal configurations depending on two parameters are found more easily, and a significant drag and lift reduction (up to −14% drag reduction) can be reached for different freestream velocities. These results are then analyzed through wall pressure and velocity measurements in the near-wake of the bluff-body with and without control. It appears that the largest drag and lift reduction is clearly associated to a strong increase of the size of the recirculation bubble over the rear slant. Investigation of the velocity field in a cross-section downstream the model reveals that, in the same time, the intensity of the longitudinal trailing vortices is strongly reduced, suggesting that the drag reduction is due to the breakdown of the balance between the separation bubble and the longitudinal vortices. It demonstrates that for low aspect ratio 3D bluff-bodies, like road vehicles, the flow control strategy is much different from the one used on airfoils: an early separation of the boundary layer can lead to a significant drag reduction if the circulation of the trailing vortices is reduced.

[1]  Contrôle d'écoulement en Aérodynamique automobile , 2009 .

[2]  Jürgen Kompenhans,et al.  Particle Image Velocimetry - A Practical Guide (2nd Edition) , 2007 .

[3]  Azeddine Kourta,et al.  Analysis and control of the near-wake flow over a square-back geometry , 2009 .

[4]  P. Luchini,et al.  Structural sensitivity of the first instability of the cylinder wake , 2007, Journal of Fluid Mechanics.

[5]  Jean-François Beaudoin,et al.  Drag reduction of a bluff body using adaptive control methods , 2006 .

[6]  John Kim,et al.  Control of turbulent boundary layers , 2003 .

[7]  Jean-François Beaudoin,et al.  Drag and lift reduction of a 3D bluff body using flaps , 2008 .

[8]  Michele Onorato,et al.  Drag Measurement Through Wake Analysis , 1984 .

[9]  W. Hucho,et al.  Aerodynamics of Road Vehicles , 1987 .

[10]  Charles Dalton,et al.  The Suppression of Lift on a Circular Cylinder due to Vortex Shedding at Moderate Reynolds Numbers , 2001 .

[11]  In Won Lee,et al.  Effect of spanwise-varying local forcing on turbulent separated flow over a backward-facing step , 1998 .

[12]  Roger Temam,et al.  DNS-based predictive control of turbulence: an optimal benchmark for feedback algorithms , 2001, Journal of Fluid Mechanics.

[13]  Frank T. Smith,et al.  Theoretical prediction and design for vortex generators in turbulent boundary layers , 1994, Journal of Fluid Mechanics.

[14]  L. Lourenço Particle Image Velocimetry , 1989 .

[15]  N. So On the breakdown of boundary layer streaks , 2022 .

[16]  Israel J Wygnanski,et al.  The control of flow separation by periodic excitation , 2000 .

[18]  Non-linear modulation of a boundary layer induced by vortex generators , 2008 .

[19]  J. Aider,et al.  Base Flow Modification by Streamwise Vortices: Application to the Control of Separated Flows , 2006 .

[20]  Patrick Gilliéron,et al.  Modelling of stationary three-dimensional separated air flows around an Ahmed reference model , 1999 .

[21]  S. R. Ahmed Influence of Base Slant on the Wake Structure and Drag of Road Vehicles , 1983 .

[22]  J. Eaton,et al.  The effects of wall roughness on the separated flow over a smoothly contoured ramp , 2002 .

[23]  John C. Lin,et al.  Review of research on low-profile vortex generators to control boundary-layer separation , 2002 .

[24]  Gioacchino Vino,et al.  Flow structures in the near-wake of the Ahmed model , 2005 .

[25]  Jean-Luc Aider,et al.  Self-sustaining process through streak generation in a flat-plate boundary layer. , 2009, Physical review letters.

[26]  Markus Raffel,et al.  Particle Image Velocimetry: A Practical Guide , 2002 .

[27]  Fabien Anselmet,et al.  Experimental analysis of flow structures and forces on a 3D-bluff-body in constant cross-wind , 2007 .

[28]  Michel Stanislas,et al.  Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators , 2006 .

[29]  P. Moin,et al.  Large Eddy Simulation of a Road Vehicle with Drag-Reduction Devices , 2002 .

[30]  D. Allano,et al.  Cavitation as a complementary tool for automotive aerodynamics , 2004 .

[31]  K. Sreenivasan,et al.  On the formation and suppression of vortex ‘shedding’ at low Reynolds numbers , 1990, Journal of Fluid Mechanics.

[32]  Mohamed Gad-el-Hak,et al.  Separation control - Review , 1991 .

[33]  Patrick Gilliéron,et al.  Aerodynamic Drag Reduction by Synthetic Jet: A 2D Numerical Study Around a Simplified Car , 2006 .

[34]  Chang Lin,et al.  Characteristics of horseshoe vortex system near a vertical plate–base plate juncture , 2002 .

[35]  Gunther Ramm,et al.  Some salient features of the time - averaged ground vehicle wake , 1984 .

[36]  R. Joslin Aircraft laminar flow control , 2000 .