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Augmentation of heat transfer by subsonic diffusion at a nearly separated stateMeasurements of mean velocity, turbulence intensity, and wall heat transfer were obtained in a 13 deg total angle of divergence conical diffuser coupled to a constant diameter recovery section. The results indicated that the boundary layer was in a nearly separated state. Turbulence intensity levels approaching 0.4 were observed in the latter stages of diffusion. The convective heat transfer was always equal to or higher than corresponding values for fully developed pipe flow at the same Reynolds number. The augmentation in heat transfer was greatest during the latter stages of diffusion where the Stanton number was nearly three times the pipe flow value.
Document ID
19730002540
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Boldman, D. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-2677
E-7082
Report Number: NASA-TM-X-2677
Report Number: E-7082
Accession Number
73N11267
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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