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Hachimi Fellouah

Researcher at Université de Sherbrooke

Publications -  60
Citations -  1078

Hachimi Fellouah is an academic researcher from Université de Sherbrooke. The author has contributed to research in topics: Turbulence & Reynolds number. The author has an hindex of 11, co-authored 50 publications receiving 842 citations. Previous affiliations of Hachimi Fellouah include Queen's University & École polytechnique de l'université de Nantes.

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On the use of numerical modelling for near-field pollutant dispersion in urban environments − A review

TL;DR: The studies performed during the past years on the wind-flow field around buildings are reviewed and errors that can produce poor results when numerically modelling wind flow and dispersion fields around buildings in urban environments are identified.
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The flow field in turbulent round free jets

TL;DR: A critical review of both experimental and computational studies of round turbulent jets is provided, beginning with the work of Tollmien (1926). as discussed by the authors traces the history, major advances, and various stages that the research community went through over the past 85-odd years, from statistical analyses through to the use of conditional sampling, proper orthogonal decomposition and structural eduction methods.
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Reynolds number effects within the development region of a turbulent round free jet

TL;DR: In this article, the effect of the Reynolds number on the near and intermediate-fields region (0,⩽,x/D, ⩽ 25) of a round free jet was investigated.
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A criterion for detection of the onset of Dean instability in Newtonian fluids

TL;DR: In this paper, the effects of the curvature ratio and aspect ratio on the stability of laminar secondary flow in 180° curved channels were studied experimentally and numerically.
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The velocity spectra and turbulence length scale distributions in the near to intermediate regions of a round free turbulent jet

TL;DR: In this paper, the velocity spectra of a round free turbulent jet were measured at Reynolds numbers ReD based on the jet exit mean velocity and the nozzle diameter, between 6000 and 100,000.