NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Low-Reynolds-number effects in a fully developed turbulent channel flowLow-Reynolds-number effects are observed in the inner region of a fully developed turbulent channel flow, using data obtained either from experiments or by direct numerical simulations. The Reynolds-number influence is observed on the turbulence intensities and to a lesser degree on the average production and dissipation of the turbulent energy. In the near-wall region, the data confirm Wei and Willmarth's (1989) conclusion that the Reynolds stresses do not scale on wall variables. One of the reasons proposed to account for this behavior, namely, the 'geometry' effect or direct interaction between inner regions on opposite walls, was investigated in some detail by introducing temperature at one of the walls, both in experiment and simulation. Although the extent of penetration of thermal excursions into the opposite side of the channel can be significant at low Reynolds numbers, the contribution these excursions make to the Reynolds shear stress and the spanwise vorticity in the opposite wall region is negligible. In the inner region, spectra and cospectra of the velocity fluctuations u and v change rapidly with the Reynolds number, the variations being mainly confined to low wavenumbers in the u spectrum.
Document ID
19920048843
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Antonia, R. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Teitel, M.
(Newcastle, University Australia)
Kim, J.
(NASA Ames Research Center Moffett Field, CA, United States)
Browne, L. W. B.
(Newcastle, University Australia)
Date Acquired
August 15, 2013
Publication Date
March 1, 1992
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 236
ISSN: 0022-1120
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92A31467
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available