An experimental investigation of water flow through an abrupt circular-channel expansion is described over a Reynolds number range between 20 and 4200. The shear layer between the central jet and the reverse flow region along the wall downstream behaved differently in the various flow regimes that were observed. With increasing Reynolds number these regimes changed progressively from a laminar flow to an unstable vortex sheetlike flow and then to a more random fluctuating flow. The distance between the step and the reattachment location downstream correspondingly increased, reached a maximum, and then decreased. Of particular significance are the shear layer wave instabilities observed in the shear flow and their relationship to rettachment which apparently has not received much attention previously. Visual observations aided in understanding the results.
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September 1972
Research Papers
Shear-Layer Flow Regimes and Wave Instabilities and Reattachment Lengths Downstream of an Abrupt Circular Channel Expansion
L. H. Back,
L. H. Back
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
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E. J. Roschke
E. J. Roschke
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
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L. H. Back
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
E. J. Roschke
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
J. Appl. Mech. Sep 1972, 39(3): 677-681 (5 pages)
Published Online: September 1, 1972
Article history
Received:
February 8, 1971
Revised:
July 22, 1971
Online:
July 12, 2010
Citation
Back, L. H., and Roschke, E. J. (September 1, 1972). "Shear-Layer Flow Regimes and Wave Instabilities and Reattachment Lengths Downstream of an Abrupt Circular Channel Expansion." ASME. J. Appl. Mech. September 1972; 39(3): 677–681. https://doi.org/10.1115/1.3422772
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