NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Convex curvature effects on the heated turbulent boundary layerA convexly curved and isothermally heated wall with a 45-cm radius of curvature is subjected to turbulent boundary layer flow measurements in order to determine wall heat transfer rates and mean velocity and temperature profiles. Significant curvature effects are noted, with Stanton number and skin friction coefficient reductions of 35-40 percent by comparison with flat plate values for the same momentum or enthalpy thickness Reynolds numbers. Profiles of mean velocity and temperature show a more rapid growth of the wake regions, and a shortening of the log-linear region, as a result of curvature. Turbulent Prandtl numbers deduced from the mean temperature profiles under the assumption of a wall thermal law were found to be increased by 40-50 percent by this strong convex curvature.
Document ID
19830061515
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simon, T. W.
(Minnesota, University Minneapolis, MN, United States)
Moffat, R. J.
(Stanford University Stanford, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Heat transfer 1982
Location: Munich
Start Date: September 6, 1982
End Date: September 10, 1982
Accession Number
83A42733
Funding Number(s)
CONTRACT_GRANT: NAG3-3
CONTRACT_GRANT: NSG-3124
Distribution Limits
Public
Copyright
Other

Available Downloads

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