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On the Development of Turbulent Wakes from Vortex StreetsWake development behind circular cylinders at Reynolds numbers from 40 to 10,000 was investigated in a low-speed wind tunnel. Standard hotwire techniques were used to study the velocity fluctuations. The Reynolds number range of periodic vortex shedding is divided into two distinct subranges. At R = 40 to 150, called the stable range, regular vortex streets are formed and no turbulent motion is developed. The range R = 150 to 300 is a transition range to a regime called the irregular range, in which turbulent velocity fluctuations accompany the periodic formation of vortices. The turbulence is initiated by laminar-turbulent transition in the free layers which spring from the separation points on the cylinder. This transition first occurs in the range R = 150 to 300. Spectrum and statistical measurements were made to study the velocity fluctuations. In the stable range the vortices decay by viscous diffusion. In the irregular range the diffusion is turbulent and the wake becomes fully turbulent in 40 to 50 diameters downstream. It was found that in the stable range the vortex street has a periodic spanwise structure. The dependence of shedding frequency on velocity was successfully used to measure flow velocity. Measurements in the wake of a ring showed that an annular vortex street is developed.
Document ID
19930083620
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Roshko, Anatol
(California Institute of Technology)
Date Acquired
August 16, 2013
Publication Date
March 1, 1953
Subject Category
Aerodynamics
Report/Patent Number
NACA-TN-2913
Report Number: NACA-TN-2913
Accession Number
93R12910
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW, SUBSONIC
FLOW, VISCOUS
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