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Near-wall modelling of compressible turbulent flowsWork was carried out to extend the near-wall models formulated for the incompressible Reynolds stress equations to compressible flows. The idea of splitting the compressible dissipation function into a solenoidal part that is not sensitive to changes of compressibility indicators and a compressible part that is directly affected by these changes is adopted. This means that all models involving the dissipation rate could be expressed in terms of the solenoidal dissipation rate and an equation governing its transport could be formulated to close the set of compressible Reynolds stress equations. The near-wall modelling of the dissipation rate equation is investigated and its behavior near a wall is studied in detail using k-epsilon closure. It is found that all existing modelled equations give the wrong behavior for the dissipation rate near a wall. Improvements are suggested and the resultant behavior is found to be in good agreement with near-wall data. Furthermore, the present modified k-epsilon closure is used too calculate a flat plate boundary layer and the results are compared with four existing k-epsilon closures. These comparisons show that all closures tested give essentially the same flow properties, except in a region very close to the wall. In this region, the present k-epsilon closure calculations are in better agreement with measurements and direct simulation data; in particular, the behavior of the dissipation rate.
Document ID
19900018342
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
So, Ronald M. C.
(Arizona State Univ. Tempe, AZ, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:186961
NASA-CR-186961
Accession Number
90N27658
Funding Number(s)
CONTRACT_GRANT: NAG1-1080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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