Evolution of swirling flow in a circular pipe after a vane swirler at moderate Reynolds numbers

The experimental results on the swirling flow structure behind a vane swirler in a smooth pipe at an axial flow Reynolds number varying within Re = 240 – 1640 are presented. A change in the degree of flow swirl along the pipe length is analyzed as a function of the Reynolds number. The main patterns in the evolution of the profiles of longitudinal and circumferential velocity components and the distribution of the root-mean-square fluctuations of the longitudinal velocity component with increasing distance from the swirler are determined. It is shown that at Re = 1640, flow instability develops in the pipe, which is a consequence of the formation of a reverse flow region on the pipe axis in the immediate vicinity of the swirler. The influence of flow swirl on the appearance of signs of a local laminar-turbulent transition in vicinity of the pipe axis and near its wall is analyzed (a sharp increase in the root-mean-square velocity fluctuations with increasing Reynolds number and the appearance of intermittency in the flow velocity oscillograms). It has been established that in the near-wall region, local turbulence of the flow is caused by the interaction between the swirler vane wakes and the wall.

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Publication Details

Journal
Thermophysics and Aeromechanics
Published
2026-05-14
DOI
https://doi.org/10.1134/s0869864325040031
Primary Topic
Heat Transfer Mechanisms
Type
article
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article

Evolution of swirling flow in a circular pipe after a vane swirler at moderate Reynolds numbers

В.М. Молочников, N. D. Pashkova, A. A. Paereliy
Thermophysics and Aeromechanics
Heat Transfer Mechanisms
article

Evolution of swirling flow in a circular pipe after a vane swirler at moderate Reynolds numbers

В.М. Молочников, N. D. Pashkova, A. A. Paereliy
article en

Abstract

The experimental results on the swirling flow structure behind a vane swirler in a smooth pipe at an axial flow Reynolds number varying within Re = 240 – 1640 are presented. A change in the degree of flow swirl along the pipe length is analyzed as a function of the Reynolds number. The main patterns in the evolution of the profiles of longitudinal and circumferential velocity components and the distribution of the root-mean-square fluctuations of the longitudinal velocity component with increasing distance from the swirler are determined. It is shown that at Re = 1640, flow instability develops in the pipe, which is a consequence of the formation of a reverse flow region on the pipe axis in the immediate vicinity of the swirler. The influence of flow swirl on the appearance of signs of a local laminar-turbulent transition in vicinity of the pipe axis and near its wall is analyzed (a sharp increase in the root-mean-square velocity fluctuations with increasing Reynolds number and the appearance of intermittency in the flow velocity oscillograms). It has been established that in the near-wall region, local turbulence of the flow is caused by the interaction between the swirler vane wakes and the wall.

Thermophysics and AeromechanicsVol. 32(4)
Kazan State Technical University named after A. N. Tupolev (RU), Kazan Scientific Center (RU)
Openalex Percentile: Top 8%
Heat Transfer Mechanisms
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