Numerical analysis of parallel jet-in-crossflow

The parallel twin jet-in-crossflow (PJICF) configuration is a variant of the heavily-studied single jet-in-crossflow (SJICF) configuration. A lack of computational studies on the near-field dynamics of the PJICF prompted this study. Insights on the trajectory and counter-rotating vortex pairs were d...

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Main Author: Lim, Avion
Other Authors: Chan Wai Lee
Format: Final Year Project
Language:English
Published: 2019
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Online Access:http://hdl.handle.net/10356/78639
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-786392023-03-04T18:29:54Z Numerical analysis of parallel jet-in-crossflow Lim, Avion Chan Wai Lee New Tze How Daniel School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering::Fluid mechanics The parallel twin jet-in-crossflow (PJICF) configuration is a variant of the heavily-studied single jet-in-crossflow (SJICF) configuration. A lack of computational studies on the near-field dynamics of the PJICF prompted this study. Insights on the trajectory and counter-rotating vortex pairs were derived from a steady Reynolds-Averaged Navier Stokes computational model of the PJICF. The jet trajectories had discrepancies with that of empirical studies, with only trajectories at low velocity ratios providing good convergence with experiments. Asymmetry in the jet trajectories was observed to decrease with increasing separation distance and decreasing velocity ratios. The trajectory scaling equation by Pratt and Baines’ for SJICF configuration showed good correlation with the PJICF configuration. The counter-rotating vortex pairs produced also provided good insight into the near-field dynamics and coincided well with empirical studies, with the inner vortices from each jet cancelling each other out very early on in the flow at smaller separation distances. An exploration of the symmetry boundary condition along the symmetry plane of the PJICF configuration also yielded good agreement compared with full mesh results in both trajectory and counter-rotating vortex pairs; the only deviations being found in highly asymmetric cases with low separation distance and high velocity ratio. Bachelor of Engineering (Aerospace Engineering) 2019-06-25T02:15:44Z 2019-06-25T02:15:44Z 2019 Final Year Project (FYP) http://hdl.handle.net/10356/78639 en Nanyang Technological University 51 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering::Fluid mechanics
spellingShingle DRNTU::Engineering::Mechanical engineering::Fluid mechanics
Lim, Avion
Numerical analysis of parallel jet-in-crossflow
description The parallel twin jet-in-crossflow (PJICF) configuration is a variant of the heavily-studied single jet-in-crossflow (SJICF) configuration. A lack of computational studies on the near-field dynamics of the PJICF prompted this study. Insights on the trajectory and counter-rotating vortex pairs were derived from a steady Reynolds-Averaged Navier Stokes computational model of the PJICF. The jet trajectories had discrepancies with that of empirical studies, with only trajectories at low velocity ratios providing good convergence with experiments. Asymmetry in the jet trajectories was observed to decrease with increasing separation distance and decreasing velocity ratios. The trajectory scaling equation by Pratt and Baines’ for SJICF configuration showed good correlation with the PJICF configuration. The counter-rotating vortex pairs produced also provided good insight into the near-field dynamics and coincided well with empirical studies, with the inner vortices from each jet cancelling each other out very early on in the flow at smaller separation distances. An exploration of the symmetry boundary condition along the symmetry plane of the PJICF configuration also yielded good agreement compared with full mesh results in both trajectory and counter-rotating vortex pairs; the only deviations being found in highly asymmetric cases with low separation distance and high velocity ratio.
author2 Chan Wai Lee
author_facet Chan Wai Lee
Lim, Avion
format Final Year Project
author Lim, Avion
author_sort Lim, Avion
title Numerical analysis of parallel jet-in-crossflow
title_short Numerical analysis of parallel jet-in-crossflow
title_full Numerical analysis of parallel jet-in-crossflow
title_fullStr Numerical analysis of parallel jet-in-crossflow
title_full_unstemmed Numerical analysis of parallel jet-in-crossflow
title_sort numerical analysis of parallel jet-in-crossflow
publishDate 2019
url http://hdl.handle.net/10356/78639
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