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Validation of three-dimensional incompressible spatial direct numerical simulation code: A comparison with linear stability and parabolic stability equation theories for boundary-layer transition on a flat plateSpatially evolving instabilities in a boundary layer on a flat plate are computed by direct numerical simulation (DNS) of the incompressible Navier-Stokes equations. In a truncated physical domain, a nonstaggered mesh is used for the grid. A Chebyshev-collocation method is used normal to the wall; finite difference and compact difference methods are used in the streamwise direction; and a Fourier series is used in the spanwise direction. For time stepping, implicit Crank-Nicolson and explicit Runge-Kutta schemes are used to the time-splitting method. The influence-matrix technique is used to solve the pressure equation. At the outflow boundary, the buffer-domain technique is used to prevent convective wave reflection or upstream propagation of information from the boundary. Results of the DNS are compared with those from both linear stability theory (LST) and parabolized stability equation (PSE) theory. Computed disturbance amplitudes and phases are in very good agreement with those of LST (for small inflow disturbance amplitudes). A measure of the sensitivity of the inflow condition is demonstrated with both LST and PSE theory used to approximate inflows. Although the DNS numerics are very different than those of PSE theory, the results are in good agreement. A small discrepancy in the results that does occur is likely a result of the variation in PSE boundary condition treatment in the far field. Finally, a small-amplitude wave triad is forced at the inflow, and simulation results are compared with those of LST. Again, very good agreement is found between DNS and LST results for the 3-D simulations, the implication being that the disturbance amplitudes are sufficiently small that nonlinear interactions are negligible.
Document ID
19920021052
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Joslin, Ronald D.
(NASA Langley Research Center Hampton, VA, United States)
Streett, Craig L.
(NASA Langley Research Center Hampton, VA, United States)
Chang, Chau-Lyan
(High Technology Corp. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.60:3205
NASA-TP-3205
L-17026
Report Number: NAS 1.60:3205
Report Number: NASA-TP-3205
Report Number: L-17026
Accession Number
92N30295
Funding Number(s)
PROJECT: RTOP 505-59-50-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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