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|a Y 3.N 21/5:6/4231
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|a NACA TN 4231
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1 |
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|a Smith, Donald W.
|0 http://id.loc.gov/authorities/names/no2008161278
|1 http://isni.org/isni/0000000073098804.
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|a Skin-friction measurements in incompressible flow /
|c by Donald W. Smith amd John H. Walker.
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|a Washington :
|b National Advisory Committee for Aeronautics,
|c [1958]
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| 300 |
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|a 67 pages :
|b illustrations ;
|c 27 cm.
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| 336 |
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|a text
|b txt
|2 rdacontent.
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|a unmediated
|b n
|2 rdamedia.
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|a volume
|b nc
|2 rdacarrier.
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|a National Advisory Committee for Aeronautics. Technical Note ;
|v 4231.
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|a Cover title.
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|a "March 1958."
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|a NACA TN Number 4231.
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|a Prepared at Ames Aeronautical Laboratory.
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|a Includes bibliographical references (pages 18-19)
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|a Experiments have been conducted to measure in incompressible flow the local surface-shear stress and the average skin-friction coefficient for a turbulent boundary layer on a smooth, flat plate having zero pressure gradient. The local surface-shear stress was measured by a floating-element skin-friction balance and also by a calibrated total head tube located on the surface of the test wall. The average skin-friction coefficient was obtained from boundary-layer velocity profiles. The boundary-layer profiles were also used to determine the location of the virtual origin of the turbulent boundary layer. Data were obtained for a range of Reynolds numbers from 1 million to about 45 million with an attendant change in Mach number from 0.11 to 0.32.
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|a committed to retain
|c 20230101
|d 20480101
|5 CoU
|f Alliance Shared Trust
|u https://www.coalliance.org/shared-print-archiving-policies.
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|a Skin friction (Aerodynamics)
|x Measurement.
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| 650 |
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|a Compressibility.
|0 http://id.loc.gov/authorities/subjects/sh85029439.
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|a Turbulent boundary layer.
|0 http://id.loc.gov/authorities/subjects/sh85138754.
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|a Plates (Engineering)
|x Testing.
|0 http://id.loc.gov/authorities/subjects/sh2010106585.
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|a Compressibility.
|2 fast
|0 (OCoLC)fst00871872.
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|a Plates (Engineering)
|x Testing.
|2 fast
|0 (OCoLC)fst01066796.
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|a Skin friction (Aerodynamics)
|x Measurement.
|2 fast
|0 (OCoLC)fst01120143.
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|a Turbulent boundary layer.
|2 fast
|0 (OCoLC)fst01159225.
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|a Walker, John H.
|0 http://id.loc.gov/authorities/names/n83005935.
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| 710 |
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|a United States.
|b National Advisory Committee for Aeronautics.
|0 http://id.loc.gov/authorities/names/n79060141
|1 http://isni.org/isni/0000000106642010.
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| 830 |
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|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 4231.
|0 http://id.loc.gov/authorities/names/no2009017392.
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|a MARS - RDA ENRICHED
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|b 05-01-17
|c 04-19-17
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|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Offsite
|d PASCAL Offsite
|e Y 3.N 21/5:6/4231
|h Superintendent of Documents classification
|i document
|m P204092401007
|n 1
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