This thesis investigates the influence of Cylindrical Distributed Roughness Elements (polka-dots) on cylinder flow, with a focus on potential applications in sports aerodynamics. The primary goals are twofold: to explore the mechanism behind tripping and to analyse how the dimensions (height, width, spacing) of polka-dots affect flow characteristics. The research employs an experimental approach, utilising balance measurements to quantify drag within the relevant Reynolds number range experienced by the limbs of speed-skaters. Additionally, Particle Image Velocimetry (PIV) measurements are conducted to examine the boundary layer and wake flow, revealing insights into how different polka-dot geometries impact flow characteristics.

11 polka-dot configurations were tested wherein the polka-dot height, diameter and spanwise (flow-normal) spacing was varied. Two PIV domains were imaged: the boundary layer flow before and after the polka-dot (covering an azimuthal range of about 40◦ of the circular profile), and the wake domain of the cylinder (about 2 diameters into the downstream flow). The boundary layer flow images were used to characterise the flow seen by the polka-dot array, and how it is affected by changes in the polka-dot geometry. The wake domain PIV imagery was used to examine the shape and dimensions of the cylinder wake.

Among the 11 tested polka-dot configurations, 10 effectively triggered drag reduction to varying extents within the relevant regime. The minimum drag coefficient was achieved by the configuration with the polka-dots of greatest diameter. It was also seen that increasing polka-dot height is likely to cause premature separation which is further exacerbated by a narrower polka-dot spacing. In general, results indicate that shorter and wider polka-dots cause transition at lower Reynolds numbers, and a greater reduction in drag occurs when transition takes place at higher Reynolds numbers. Polka-dots placed in closer proximity initiate flow tripping earlier, while wider spacing results in more substantial drag reduction. However, it is observed that the polka-dots, when spaced closer together, see a lower flow velocity for the same polka-dot height and may lead to premature separation.

In terms of the wake width, a high linear correlation is seen between the measured wake width and the measured coefficient of drag (r² ≈ 0.9). It is also seen that for drag coefficient values close to the minimum drag coefficient value, the wake width sees minimal change. The change in wake geometry is then seen as a change in the wake tapering (downstream decrease of the wake width) and the streamwise wake length. Therefore, a larger wake imaging domain in the streamwise direction is likely to allow for a more accurate correlation of the wake geometry and the drag coefficient.

While the study offers valuable insights, several recommendations are put forth for further research. Expanding the wake imaging domain is suggested to enhance correlations with the drag coefficient, and investigating spanwise flow variations would provide deeper insight into the tripping mechanism.

Wind tunnel investigations of cycling aerodynamics are conducted in air streams that are designed to have minimum turbulence. This is not representative of the true, turbulent wind environment encountered by a track cyclist in an indoor velodrome. The goal of this thesis, broadly speaking, is to assess the effects of this turbulence on cycling aerodynamics.
To address this question, two experimental campaigns were conducted. The first consisted of track measurements, to measure the turbulence intensities and spectra encountered in an indoor velodrome, by an isolated cyclist and by a cyclist in the far wake of another. This turbulence data was collected using a three-hole pressure probe. In the case of an isolated cyclist, it was observed that the airflow was dependent on the cyclist's location on track. A spectral analysis also revealed the presence of periodic components to the airflow, a result of the cyclist's cadence. When riding in the far wake of another cyclist, the turbulence encountered was stronger when the distance of separation got smaller.
The second experimental campaign was conducted in the wind tunnel. First, the measured track turbulence intensities and spectra were simulated using grids, for small scale, high frequency turbulence, and large obstacles, for large scale, low frequency turbulence. Once the simulated turbulence matched the track turbulence to acceptable levels, its effects on the drag of a cylinder model, representative of the cyclist's limb, were assessed. These drag measurements were conducted using an external force balance. It was found that for a smooth surfaced cylinder, free-stream turbulence was enough to trigger flow transitions and cause a reduction in the measured drag. For a rough surfaced cylinder, increasing the turbulence triggered flow transition earlier, and led to an increased Reynolds number range for the critical flow regime. It was also seen that large scale turbulence did not have a significant effect of the drag of the cylinder.

The importance of aerodynamic efficiency in the cycling sport is well known. Simple calculations demonstrate the considerable impact of just a few percentages in drag savings on the outcome of a competition where the margins can be incredibly small. Achieving a drag reduction can, however, be challenging as the flow topology of a cyclist is extremely complex. Nonetheless, the manipulation of flow structures in other research areas is proven to be an effective method for reducing aerodynamic resistance. Hence, the potential of achieving a drag reduction for a cyclist in a time trial position through the manipulation of the 3D flow topology is investigated.

Two devices are introduced named the Hip Vortex Control (HVC) and wingsuit aiming to reduce the streamwise vorticity at the hips and upper arms respectively. A reduction of a crosswind-dependent weighted drag area of -1.35% for the HVC and -5.45% for the wingsuit is measured experimentally. Computational Fluid Dynamics (CFD) simulations and robotic volumetric Particle Tracking Velocimetry (PTV) provide the trends in the drag-reducing mechanisms. The HVC promotes separation on the lower back of the cyclist, reducing the presence of the hip vortices leading to an increase of the pressure on the lower back. The wingsuit limits the formation of the streamwise vortices around the upper arms, slightly increasing the wake and increasing the pressure on the upper arms resulting in the drag reduction.

The numerical and experimental results largely agree on the variations in the flow topology for each configuration. The results indicate that a reduction in streamwise vorticity in the wake of a bluff body can reduce the drag considerably. Both devices lead to an expansion of the wake which should be kept to a minimum to effectively reduce the drag. The results motivate the continuation of the research into the reduction of streamwise vortices in the development of cycling equipment and in other high-velocity sports.