Analytical, numerical, and experimental results on turbulent boundary layers

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086 0 ⊔ ‡aD 301.45/33: 76-062
100 1 ⊔ ‡aWhitfield, David L., ‡eauthor.
245 1 0 ‡aAnalytical, numerical, and experimental results on turbulent boundary layers / ‡cDavid L. Whitfield.
264 ⊔ 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1976.
300 ⊔ ⊔ ‡a102 pages : ‡billustrations ; ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
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490 0 ⊔ ‡aAEDC-TR ; ‡v76-062
500 ⊔ ⊔ ‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
500 ⊔ ⊔ ‡aFinal Report: September 1974 -- January 1976."
500 ⊔ ⊔ ‡a"July 1976."
504 ⊔ ⊔ ‡aIncludes bibliographic references (page 59).
520 ⊔ ⊔ ‡aThis report describes the results of analytical, numerical, and experimental investigations of incompressible and compressible boundary layers. The subjects considered are (1) Laminar and/or turbulent numerical boundary-layer calculations in which the Reynolds stress is related to the turbulent kinetic energy; (2) an analytical investigation of turbulence near a wall which is not founded on classical mixing-length theory; (3) analytical solutions for relating velocity and temperature throughout turbulent boundary layers for nonunity Prandtl numbers; (4) a description of the data reduction of pitot pressure measurements utilizing these analytical results, and (5) the application of the numerical and analytical results to the analysis of turbulent boundary-layer measurements made in the Propulsion Wind Tunnel Facility (PWT).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aReynolds number.
650 ⊔ 0 ‡aLaminar boundary layer.
650 ⊔ 0 ‡aTurbulent boundary layer.
710 2 ⊔ ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
710 2 ⊔ ‡aARO, Inc., ‡esponsor.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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