NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A Numerical simulation of transition in plane channel flowA numerical simulation of the final stages of transition to turbulence in plane channel flow at a Reynolds number of 7500 is described. 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 32 by 33 by 32 grid. Solutions indicate the existence of structures similar to those observed in the laboratory and which are characteristic of various stages of transition that lead to final breakdown. Details of the resulting flow field after breakdown indicate the evolution of streak-like formations found in turbulent flows. Although the flow field does approach a steady state (turbulent channel flow), implementation of subgrid-scale terms are necessary to obtain proper turbulent statistics.
Document ID
19820024760
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goglia, G.
(Old Dominion Univ. Norfolk, VA, United States)
Biringen, S.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:169322
NASA-CR-169322
Report Number: NAS 1.26:169322
Report Number: NASA-CR-169322
Accession Number
82N32636
Funding Number(s)
CONTRACT_GRANT: NAG1-228
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available