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Turbulent boundary layer over solid and porous surfaces with small roughnessThe wind tunnel models and instrumentation used as well as data reduction and error analysis techniques employed are described for an experimental study conducted to measure directly skin friction and obtain profiles of mean velocity, axial and normal turbulence intensity, and Reynolds stress in the untripped boundary on a large diameter axisymmetric body. Results are given for such a body with a (1) smooth, solid surface; (2) a sandpaper roughened, solid surface; (3) a sintered metal, porous surface; (4) a ""smooth'' performated titanium surface; (5) a rough, solid surface made of fine diffusion bonded screening; and (6) a rough, porous surface made of the same screening. The roughness values were in low range (k+ 5 to 7) just above what is normally considered ""hydraulically smooth''. Measurements were taken at several axial locations and tow or normal stream freestream velocities, 45.1 m/sec and 53.5 m/sec.
Document ID
19830002113
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kong, F. Y.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Schetz, J. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Collier, F.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:3612
NASA-CR-3612
Report Number: NAS 1.26:3612
Report Number: NASA-CR-3612
Accession Number
83N10383
Funding Number(s)
CONTRACT_GRANT: NAG1-119
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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