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Turbulent boundary layer over porous surfaces with different surface geometriesThe turbulent boundary layer over three porous walls with different surface geometries was studied in order to investigate the individual influences of porosity and small roughness, as well as their combined effects, on turbulent boundary layer behavior. The tests were conducted in a 2 m x 2 m tunnel on a large axisymmetric model at speeds corresponding to Re(L) = 5,000,000-6,000,000. The development of the turbulent boundary layer was compared for that of sintered metal, bonded screening, and perforated sheet and then to that for the flow over a solid smooth wall and a solid, sand-roughened wall. The comparisons reveal that the effect of porosity is to shift the logarithmic region of the wall law down by a certain amount from the solid wall results and to increase the skin friction values by about 30-40%. The downward shift of the logarithmic region of the wall law and the increase of the skin friction value by the combined effects of small roughness and porosity are found to be roughly the sum of their individual effects.
Document ID
19820034207
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kong, F. Y.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Schetz, J. A.
(Virginia Polytechnic Institute and State University Blacksburg, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 82-0030
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Orlando, FL
Start Date: January 11, 1982
End Date: January 14, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A17742
Distribution Limits
Public
Copyright
Other

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