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Revuelta Bayod, Antonio, Sánchez Pérez, Antonio Luis and Liñán Martínez, Amable (2002). Confined axisymmetric laminar jets with large expansion ratios. "Journal of Fluid Mechanics", v. 456 ; pp. 319-352. ISSN 0022-1120.
Title: | Confined axisymmetric laminar jets with large expansion ratios |
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Author/s: |
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Item Type: | Article |
Título de Revista/Publicación: | Journal of Fluid Mechanics |
Date: | 2002 |
ISSN: | 0022-1120 |
Volume: | 456 |
Subjects: | |
Freetext Keywords: | boundary layers; jets; laminar flow; Navier Stokes equations; pipe flow; stratified flow; vortices; confined axisymmetric laminar jets; large expansion ratios; steady round laminar jet; coaxial duct; jet Reynolds number; downstream flow; flow field; slender unconfined jet; constant momentum flux; jet entrainment; slow backflow motion; momentum exchange; toroidal vortex; nonslender transition zone; recirculating flow; boundary layer approximation; nonslender flows |
Faculty: | E.T.S.I. Aeronáuticos (UPM) |
Department: | Motopropulsión y Termofluidodinámica [hasta 2014] |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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This paper investigates the steady round laminar jet discharging into a coaxial duct when the jet Reynolds number, Re/sub j/, is large and the ratio of the jet radius to the duct radius, epsiv, is small. The analysis considers the distinguished double limit in which the Reynolds number Re/sub a/=Re/sub j/epsiv for the final downstream flow is of order unity, when four different regions can be identified in the flow field. Near the entrance, the outer confinement exerts a negligible influence on the incoming jet, which develops as a slender unconfined jet with constant momentum flux. The jet entrains outer fluid, inducing a slow backflow motion of the surrounding fluid near the backstep. Further downstream, the jet grows to fill the duct, exchanging momentum with the surrounding recirculating flow in a slender region where the Reynolds number is still of the order of Re/sub j/. The streamsurface bounding the toroidal vortex eventually intersects the outer wall, in a non-slender transition zone to the final downstream region of parallel streamlines. In the region of jet development, and also in the main region of recirculating flow, the boundary-layer approximation can be used to describe the flow, while the full Navier-Stokes equations are needed to describe the outer region surrounding the jet and the final transition region, with Re/sub a/=Re/sub j/epsiv entering as the relevant parameter to characterize the resulting non-slender flows.
Item ID: | 861 |
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DC Identifier: | https://oa.upm.es/861/ |
OAI Identifier: | oai:oa.upm.es:861 |
Official URL: | http://journals.cambridge.org/action/displayJourna... |
Deposited by: | Archivo Digital UPM |
Deposited on: | 16 Feb 2008 |
Last Modified: | 20 Apr 2016 06:34 |