Abstract

The control of bluff-body wakes for reduced drag and enhanced stability has traditionally relied on the so-called direct-wake control approach. By the use of actuators or passive devices, one can manipulate the aerodynamic loads that act on the rear of the model. An alternative approach for the manipulation of the flow is to move the position of the actuator upstream, hence interacting with an easier-to-manipulate boundary layer. The present paper comprises a bluff-body flow study via large-eddy simulations to investigate the effectiveness of an upstream actuator (positioned at the leading edge) with regard to the manipulation of the wake dynamics and its aerodynamic loads. A rectangular cylinder with rounded leading edges, equipped with actuators positioned at the front curvatures, is simulated at $Re=40\,000$ . A genetic algorithm (GA) optimization is performed to find an effective actuation that minimizes drag. It is shown that the GA selects superharmonic frequencies of the natural vortex shedding. Hence, the induced disturbances, penetrating downstream in the wake, significantly reduce drag and lateral instability. A comparison with a side-recirculation-suppression approach is also presented, the latter case being worse in terms of reduced drag (only 8 % drag reduction achieved), despite the total suppression of the side recirculation bubble. In contrast, the GA optimized case contributes to a 20 % drag reduction with respect to the unactuated case. In addition, the large drag reduction is associated with a reduced shedding motion and an improved lateral stability.

Highlights

  • The control of the flow surrounding bluff bodies can greatly improve their aerodynamic performance

  • In contrast to the work of Li et al (2017), the present study aims to identify a viable way to control the wake only by intervention on the upstream leading-edge boundary layers (BLs)

  • An actuation that may effectively control the wake dynamics is preferable compared to a localized control, if the overall drag reduction represents the main deliverable of an optimization study

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Summary

Introduction

The control of the flow surrounding bluff bodies can greatly improve their aerodynamic performance. This is achieved by the manipulation of the leading-edge shear flow, in order to control both the local separation (at the side of the body) and the downstream wake dynamics, reducing the global drag and improving the lateral stability This may have a strong impact on real-life applications. The first deals with bluff bodies with a movable separation point, and the second describes cases where the control directly affects the wake structures This distinction, is not suitable for the present study, where an apparent BL control (placed at the front rounded leading edge) will indirectly affect the downstream structures, penetrating into the wake and defining, to some extent, its dynamics.

Methodology and numerical set-up
Resolution and numerical schemes
The actuation strategy
The genetic algorithm optimization
Evaluation Elitism
Results
The genetic algorithm evolution
The 2-D flow topology and the effect of the actuation
The 2-D versus 3-D flow topologies
The 3-D LES grid independence study
Conclusions and future development

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