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Experimental study of vortex breakdown in a cylindrical, swirling flowThe stability of a steady, vortical flow in a cylindrical container with one rotating endwall has been experimentally examined to gain insight into the process of vortex breakdowwn. The dynamics of the flow are governed by the Reynolds number (Re) and the aspect ratio of the cylinder. Re is given by Omega R(sup 2)/nu, where Omega is the speed of rotation of the endwall, R is the cylinder radius, and nu is the kinematic viscosity of the fluid filling the cylinder. The aspect ratio is H/R, where H is the height of the cylinder. Numerical simulation studies disagree whether or not the steady breakdown is stable beyond a critical Reynolds number, Re(sub c). Previous experimental researches have considered the steady and unsteady flows near Re(sub c), but have not explored the stability of the steady breakdown structures beyond this value. In this investigation, laser induced fluorescence was utilized to observe both steady and unsteady vortex breakdown at a fixed H/R of 2.5 with Re varying around Re(sub c). When the Re of a steady flow was slowly increased beyond Re(sub c), the breakdown structure remained steady even though unsteadiness was possible. In addition, a number of hysteresis events involving the oscillation periods of the unsteady flow were noted. The results show that both steady and unsteady vortex breakdown occur for a limited range of Re above Re(sub c). Also, with increasing Re, complex flow transformations take place that alter the period at which the unsteady flow oscillates.
Document ID
19960041438
Acquisition Source
Ames Research Center
Document Type
Contractor Report (CR)
Authors
Stevens, J. L.
(Stanford Univ. CA United States)
Celik, Z. Z.
(Stanford Univ. CA United States)
Cantwell, B. J.
(Stanford Univ. CA United States)
Lopez, J. M.
(Stanford Univ. CA United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1996
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-201483
NAS 1.26:201483
Report Number: NASA-CR-201483
Report Number: NAS 1.26:201483
Accession Number
96N31382
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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