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Experimental and analytical study of a conically diffused flow with a nearly separated boundary layerTurbulence measurements were obtained in the nearly separated flow in a 13 deg total angle of divergence conical diffuser coupled to a constant area tailpipe. Air at 207 newtons per square centimeter and 308 K provided an inlet velocity of about 51 meters per second at an inlet unit Reynolds number of 63.7 million per meter. Very high longitudinal turbulence intensities accompanied the diffusion process with peak values approaching 40 percent when normalized by the local centerline velocity. Predictions of the pressure recovery coefficient using a mixing length concept were good in the early stages of diffusion. In the latter stages of diffusion satisfactory predictions of the pressure recovery were obtained with an empirical method.
Document ID
19740002212
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Boldman, D. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Neumann, H. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
E-7423
NASA-TN-D-7486
Report Number: E-7423
Report Number: NASA-TN-D-7486
Accession Number
74N10325
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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