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Heat transfer in the turbulent boundary layer with a step change in surface roughnessMeasurements of Stanton numbers, velocity profiles, temperature profiles, and turbulence intensity profiles are reported for turbulent flat plate boundary layer flows with a step change in surface roughness. The first 0.9 m length of the test surface is roughened with 1.27 mm diameter hemispheres spaced 2 base diameters apart in a staggered array. The remaining 1.5 m length is smooth. The experiments show that the step change from a rough to a smooth surface has a dramatic effect on the convective heat transfer. In many cases, the Stanton number drops below the smooth-wall correlation immediately downstream of the change in roughness. The Stanton number measurements are compared with predictions using the discrete element method with excellent results.
Document ID
19920033040
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Taylor, Robert P.
(Mississippi State Univ. Mississippi State, MS, United States)
Taylor, J. K.
(Mississippi State Univ. Mississippi State, MS, United States)
Coleman, Hugh W.
(Mississippi State University Mississippi State, United States)
Hosni, M. H.
(Kansas State University Manhattan, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ASME PAPER 91-GT-266
Accession Number
92A15664
Funding Number(s)
CONTRACT_GRANT: NAG3-1116
Distribution Limits
Public
Copyright
Other

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