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Numerical simulation of boundary-layer transitionThe transition to turbulence in boundary layers was investigated by direct numerical solution of the nonlinear, three-dimensional, incompressible Navier-Stokes equations in the half-infinite domain over a flat plate. Periodicity was imposed in the streamwise and spanwise directions. A body force was applied to approximate the effect of a nonparallel mean flow. The numerical method was spectra, based on Fourier series and Jacobi polynomials, and used divergence-free basis functions. Extremely rapid convergence was obtained when solving the linear Orr-Sommerfeld equation. The early nonlinear and three-dimensional stages of transition, in a boundary layer disturbed by a vibrating ribbon, were successfully simulated. Excellent qualitative agreement was observed with either experiments or weakly nonlinear theories. In particular, the breakdown pattern was staggered or nonstaggered depending on the disturbance amplitude.
Document ID
19840020677
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spalart, P. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-85984
A-9796
NAS 1.15:85984
Report Number: NASA-TM-85984
Report Number: A-9796
Report Number: NAS 1.15:85984
Accession Number
84N28746
Funding Number(s)
PROJECT: RTOP 505-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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