Abstract

An experimental study of bluff bodies in confinement is presented. Two Reynolds matched rigs (pipe diameters: $D=40~\text{mm}$ and $D=194~\text{mm}$) are used to derive a picture of the flow topology of the primary-shedding mode (Kármán vortex, mode-I). Confined bluff bodies create an additional spectral mode (mode-II). This is caused by the close coupling of the shedder blockage and the wall and is unique to the confined bluff-body problem. Under certain conditions, modes-I and II can interact, resulting in a lock-on, wherein the modes cease to exist at independent frequencies. The topological effects of mode interaction are demonstrated using flow visualisation. Furthermore, the scaling of mode-II is explored. The two experimental facilities span Reynolds numbers (based on the shedder diameter, $d$) $10^{4}<Re_{d}<10^{5}$ and bulk Mach numbers $0.02<M_{b}<0.4$. Bluff bodies with a constant blockage ratio ($d/D$), forebody shape and various splitter-plate lengths ($l$) and thicknesses ($t$) are used. Results indicate that the flow topology changes substantially between short ($l<d$) and long ($l>d$) tailed geometries. Surface flow visualisation indicates that the primary vortex becomes anchored on the tail when $l\gtrsim 3h$ ($2h=d-t$). This criterion prohibits the development of such a topology for short-tailed geometries. When mode interaction occurs, which it does exclusively in long-tailed cases, the tail-anchored vortex pattern is disrupted. The onset of mode-II occurs at approximately the same Reynolds number in both rigs, although the associated dimensionless frequency is principally a function of Mach number. Accordingly, mode interaction is avoided in the larger-scale rig, due to the increased separation of the modal frequencies.

Highlights

  • The vortex shedding behind unconfined bluff bodies has been extensively researched since the independent discovery of the phenomenon in the early 1900s by Henri Bénard and Theodor von Kármán; Wesfried (2006) provides a historical account

  • Spectrograms and surface-flow visualisations are used in conjunction to show that the tail anchored vortex (TAV) pattern is disrupted during mode interaction

  • Assuming that mode-II is connected to the viscous-dominated wall flow, it is sensible that the onset occurs at similar Reynolds numbers in the two rigs

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Summary

Introduction

The vortex shedding behind unconfined bluff bodies has been extensively researched since the independent discovery of the phenomenon in the early 1900s by Henri Bénard and Theodor von Kármán; Wesfried (2006) provides a historical account. They demonstrate that the dimensionless frequency undergoes a rapid increase (in some cases more than doubling) as a result of transition on the shedding body This occurs beyond a critical Reynolds number (Red 105). A recent work by Ford, Winroth & Alfredsson (2018) examined the influences of shedder geometry on vortex shedding of confined bluff bodies. Bearman (1965) presents a flow visualisation study of a low-confinement bluff body (d/D = 0.03) at Reynolds numbers relevant to the present study (104 Red 105). The authors report that similar reattachment lines were seen for tails with lengths greater than 2.9d Another flow visualisation study was made by Ruderich & Fernholz (1986) for flat-nosed bodies with very long splitter plates (l/d ≈ 30) at Red = O(104).

Experimental set-up
The CICERO rig
The NT rig
Shedder geometry and dimensions
Definitions
Primary-vortex shedding
Mode-I scaling
Mode-I topology and the effect of tail length
Topological effects of mode interaction
Mode-II
Findings
Summary and conclusions
Full Text
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