Velocity measurements and turbulence statistics of a confined isothermal swirling flow

Saad A. Ahmed*

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

50 Scopus citations

Abstract

A two-component laser Doppler velocimeter was employed to measure the flow properties of a confined, isothermal, swirling flowfield in an axisymmetric sudden expansion research combustor. A free vortex swirler was used to stir the flow at the inlet of the combustor. Measurements of mean velocities, Reynolds normal and shear stresses, and triple products were carried out at axial distances ranging from O.38H (step height) to 18H downstream of the swirler. Detailed experimental data are provided to help in the understanding of the behavior of swirling, recirculating, axisymmetric, and turbulent flows inside dump combustors. A balance of the turbulence energy equation has been performed in order to get a detailed insight into the turbulent shear layer behavior. The turbulent kinetic energy terms: production, diffusion, and convection terms were computed directly from the experimental data using central differences. The viscous dissipation term was obtained from the balance of the kinetic energy equation. The analysis of the data was successful in identifying the various areas of interest in the flowfield where different turbulent transport mechanisms dominate. In addition, the data from this study will be available for upgrading advanced numerical codes. The swirling flow streamlines data are compared with the simple dump flow and it is shown that swirl reduces the size of the corner recirculation region in addition to creating a central toroidial recirculation region. In summary, swirling enhances the production and distribution of turbulence energy in the combustro which, in turn, indicates thorough flow mixing and earlier flow recovery.

Original languageEnglish
Pages (from-to)256-264
Number of pages9
JournalExperimental Thermal and Fluid Science
Volume17
Issue number3
DOIs
StatePublished - Jul 1998

Bibliographical note

Funding Information:
This investigation was performed at Aero-propulsion and Power Directorate (WL/POPT) while the author was employed at the Wright Laboratory. The author wishes to acknowledge the financial support of AFOSR, and also KFUPM for utilizing the various facilities in preparation of the paper.

ASJC Scopus subject areas

  • General Chemical Engineering
  • Nuclear Energy and Engineering
  • Aerospace Engineering
  • Mechanical Engineering
  • Fluid Flow and Transfer Processes

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