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On the theory of the turbulent boundary layerAs a rule, a division of the turbulent boundary layer is admissible: a division into a part near the wall, where the flow is governed only by the wall effects, and into an outer part, where the wall roughness and the viscosity of the flow medium affects only the wall shearing stress occurring as boundary condition but does not exert any other influence on the flow. Both parts may be investigated to a large extent independently. Under certain presuppositions there result for the outer part "similar" solutions. The theoretical considerations give a cue how to set up, by appropriate experiments and their evaluation, generally valid connections which are required for the approximate calculation of the turbulent boundary layer according to the momentum and energy theorem.
Document ID
19930093886
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rotta, J
Date Acquired
August 16, 2013
Publication Date
February 1, 1953
Report/Patent Number
NACA-TM-1344
Report Number: NACA-TM-1344
Accession Number
93R23211
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBULENCE
SKIN FRICTION
EQUATIONS - BOUNDARY LAYER, TURBULENT
BOUNDARY LAYER - EFFECT OF SURFACE ROUGHNESS
THEORIES - BOUNDARY LAYER, TURBULENT
BOUNDARY LAYER - PLATES, EFFECT OF VISCOSITY7
BOUNDARY LAYER - EFFECT OF PRESSURE GRADIENT
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