4.7 Article

Effects of nozzle inlet size and curvature on the flow development in a bidirectional vortex chamber

Journal

PHYSICS OF FLUIDS
Volume 33, Issue 9, Pages -

Publisher

AIP Publishing
DOI: 10.1063/5.0066121

Keywords

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Funding

  1. National Science Foundation [CMMI-1761675]
  2. Hugh and Loeda Francis Chair of Excellence, Department of Aerospace Engineering, Auburn University

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The study utilized a finite-volume solver to simulate cyclonic motion in a cylindrical vortex chamber, demonstrating the accuracy of numerical simulations through comparison with theoretical results. Additionally, a parametric study systematically investigated the impact of nozzle variations on internal flow characteristics.
A finite-volume solver is used to describe the cyclonic motion in a cylindrical vortex chamber comprising eight tangential injectors and a variable nozzle size. The simulations are performed under steady, incompressible, and inviscid flow conditions with air as the working fluid. First, we apply a fine tetrahedral mesh to minimize cell skewness, particularly near injectors. Second, this mesh is converted into a polyhedral grid to improve convergence characteristics and precision. After achieving convergence, the velocity components are evaluated and compared to existing analytical solutions. We find that well-resolved numerical simulations can accurately predict the expected forced vortex behavior in the core region as well as the free vortex tail in the outer region. We also confirm that the swirl velocity remains axially invariant irrespective of the outlet radius. Similarly, we are able to ascertain that the axial and radial velocities embody the bidirectional nature of the motion. As for the computed pressure distribution, it is found to agree quite well with both theoretical formulations and experimental measurements of cyclone separators. Then using a parametric trade study, the effect of nozzle variations on the internal flow character, mantle structure, and recirculation zones is systematically investigated. Apart from the exit diameter, we find that the nozzle length and inlet curvature can substantially affect the internal flow development including the formation of backflow regions, recirculation zones, and mantle excursions. Finally, an empirical relation is constructed for the nozzle radius of curvature and shown to effectively suppress the emergence of recirculation and backflow regions. (C) 2021 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).

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