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Transition to turbulence in plane channel flowA numerical simulation of the final stages of transition to turbulence in plane channel flow is reported. Three dimensional, incompressible Navier-Stokes equations are numerically integrated to obtain the time-evolution of two and three dimensional finite amplitude disturbances. Computations are performed on the CYBER-203 vector processor for a 32x51x32 grid. Results are presented for no-slip boundary conditions at the solid walls as well as for periodic suction-blowing to simulate active control of transition by mass transfer. Solutions indicate that the method is capable of simulating the complex character of vorticity dynamics during the various stages of transition and final breakdown. In particular, evidence points to the formation of a lambda-shape vortex and the subsequent system of horseshoe vortices inclined to the main flow direction as the main elements of transition. Calculations involving suction-blowing indicate that interference with a wave of suitable phase and amplitude reduces the disturbance growth rates.
Document ID
19840008418
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Biringen, S.
(Old Dominion Univ. Norfolk, VA, United States)
Goglia, G. L.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:173149
NASA-CR-173149
Report Number: NAS 1.26:173149
Report Number: NASA-CR-173149
Accession Number
84N16486
Funding Number(s)
CONTRACT_GRANT: NAG1-228
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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