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The slow recirculating flow near the rear stagnation point of a wakeA model is suggested in which some of the important features of the circulating flow inside the two-dimensional near wake are derived by assuming a slow viscous flow. The theory considers the flow away from the body base. It is found that there is a region of constant speed merging, as we go downstream, into a region of stagnation-apex flow. The velocity returning from the rear stagnation point along the center streamline is shown to be a slowly varying function of the 'wedge-angle,' of the wake and to be roughly one half the velocity at the edge of the shear layers driving the wake-cavity flow. These results seem to be in agreement with experimental data.
Document ID
19770003544
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Abarbanel, S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
REPT-75-18
AFOSR-76-0479TR
NASA-TM-X-74156
AD-A024369
Accession Number
77N10486
Funding Number(s)
OTHER: NGR-47-102-001
PROJECT: AF PROJ. 9781
OTHER: AF-AFOSR-2370-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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