Abstract

A specific feature of three-dimensional bluff body wakes, flow bistability, is a subject of particular recent interest. This feature consists of a random flipping of the wake between two asymmetric configurations and is believed to contribute to the pressure drag of many bluff bodies. In this study we apply the modelling approach recently suggested for axisymmetric bodies by Rigaset al.(J. Fluid Mech., vol. 778, 2015, R2) to the reflectional symmetry-breaking modes of a rectilinear bluff body wake. We demonstrate the validity of the model and its Reynolds number independence through time-resolved base pressure measurements of the natural wake. Further, oscillating flaps are used to investigate the dynamics and time scales of the instability associated with the flipping process, demonstrating that they are largely independent of Reynolds number. The modelling approach is then used to design a feedback controller that uses the flaps to suppress the symmetry-breaking modes. The controller is successful, leading to a suppression of the bistability of the wake, with concomitant reductions in both lateral and streamwise forces. Importantly, the controller is found to be efficient, the actuator requiring only 24 % of the aerodynamic power saving. The controller therefore provides a key demonstration of efficient feedback control used to reduce the drag of a high-Reynolds-number three-dimensional bluff body. Furthermore, the results suggest that suppression of large-scale structures is a fundamentally efficient approach for bluff body drag reduction.

Highlights

  • For many three-dimensional wakes, a prominent feature that is believed to contribute to pressure drag is the so-called bistability

  • Concluding remarks In this paper we have demonstrated that the RSB mode of rectilinear bluff body wakes can be modelled by a nonlinear Langevin equation, in which the deterministic part describes the evolution of the large-scale structure and the stochastic part models the influence of the turbulent forcing

  • The model can be used in the design of a feedback controller that uses dynamic flaps to try to restore the naturally unstable symmetric flow condition

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Summary

Introduction

For many three-dimensional wakes, a prominent feature that is believed to contribute to pressure drag is the so-called bistability. This feature consists of an instantaneous asymmetry of the wake, even under nominally symmetric flow conditions, and a random switching between two such asymmetric states. A number of studies have examined this same feature on the body of Ahmed, Ramm & Faltin (1984) This so-called Ahmed body, shown in figures 1 and 2, provides a generic representation of a road vehicle, including the essential features of a real vehicle flow field such as three-dimensional separation and ground effect. For even higher Reynolds numbers, the flow becomes unsteady and periodic shedding starts to occur These two regimes were observed for Re > 340 and Re > 410, respectively (Grandemange et al 2012)

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