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Multigrid direct numerical simulation of the whole process of flow transition in 3-D boundary layersA new technology was developed in this study which provides a successful numerical simulation of the whole process of flow transition in 3-D boundary layers, including linear growth, secondary instability, breakdown, and transition at relatively low CPU cost. Most other spatial numerical simulations require high CPU cost and blow up at the stage of flow breakdown. A fourth-order finite difference scheme on stretched and staggered grids, a fully implicit time marching technique, a semi-coarsening multigrid based on the so-called approximate line-box relaxation, and a buffer domain for the outflow boundary conditions were all used for high-order accuracy, good stability, and fast convergence. A new fine-coarse-fine grid mapping technique was developed to keep the code running after the laminar flow breaks down. The computational results are in good agreement with linear stability theory, secondary instability theory, and some experiments. The cost for a typical case with 162 x 34 x 34 grid is around 2 CRAY-YMP CPU hours for 10 T-S periods.
Document ID
19940013084
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Liu, Chaoqun
(NASA Lewis Research Center Cleveland, OH, United States)
Liu, Zhining
(Colorado Univ. Denver., United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:106369
CMOTT-93-13
ICOMP-93-36
E-8175
NASA-TM-106369
Report Number: NAS 1.15:106369
Report Number: CMOTT-93-13
Report Number: ICOMP-93-36
Report Number: E-8175
Report Number: NASA-TM-106369
Accession Number
94N17557
Funding Number(s)
CONTRACT_GRANT: NAS1-10312
CONTRACT_GRANT: NCC3-233
PROJECT: RTOP 505-90-5K
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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