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Embedded function methods for compressible high speed turbulent flowFundamental issues relating to compressible turbulent flow are addressed. The focus has been on developing methods and testing concepts for attached flows rather than trying to force a conventional law of the wall into a zone of backflow. Although the dynamics of the near-wall flow in an attached turbulent boundary layer are relatively well documented, the dynamical features of a zone of reversed turbulent flow are not, nor are they well understood. Incompressibility introduces effects and issues that have been dealt with only marginally in the literature, therefore, the present work has been focussed on attached high-speed flows. The wall function method has been extended up through the supersonic to hypersonic speeds. Algorithms have been successfully introduced into the code that calculates the flow all the way to the wall, and testing is being carried out for progressively more complex flow situations.
Document ID
19900005182
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Walker, J. D. A.
(Lehigh Univ. Bethlehem, PA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-186131
NAS 1.26:186131
Accession Number
90N14498
Funding Number(s)
CONTRACT_GRANT: NAG1-8321
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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