NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Coherent structures in a simulated turbulent mixing layerA direct numerical simulation of a plane turbulent mixing layer has been performed. The simulation was initialized using two turbulent velocity fields obtained from direct numerical simulation of a turbulent boundary layer at momentum thickness Reynolds number 300 (Spalart, 1988). The mixing layer is allowed to evolve long enough for self-similar linear growth to occur, with the visual thickness Reynolds number reaching 14,000. The simulated flow is examined for evidence of the coherent structures expected in a mixing layer (rollers and rib vortices). Before the onset of self-similar growth, such structures are present with properties similar to the corresponding laminar or transitional structures. In the self-similar growth regime, however, only the rollers are present with no indication of rib vortices and no indication of conventional pairing. This results in a reduction of mixing and layer growth.
Document ID
19930009696
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Moser, Robert D.
(NASA Ames Research Center Moffett Field, CA, United States)
Rogers, Michael M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:103980
A-92197
NASA-TM-103980
Report Number: NAS 1.15:103980
Report Number: A-92197
Report Number: NASA-TM-103980
Accession Number
93N18885
Funding Number(s)
PROJECT: RTOP 505-59-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available