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An Approach for Dynamic GridsAn approach is presented for the generation of two-dimensional, structured, dynamic grids. The grid motion may be due to the motion of the boundaries of the computational domain or to the adaptation of the grid to the transient, physical solution. A time-dependent grid is computed through the time integration of the grid speeds which are computed from a system of grid speed equations. The grid speed equations are derived from the time-differentiation of the grid equations so as to ensure that the dynamic grid maintains the desired qualities of the static grid. The grid equations are the Euler-Lagrange equations derived from a variational statement for the grid. The dynamic grid method is demonstrated for a model problem involving boundary motion, an inviscid flow in a converging-diverging nozzle during startup, and a viscous flow over a flat plate with an impinging shock wave. It is shown that the approach is more accurate for transient flows than an approach in which the grid speeds are computed using a finite difference with respect to time of the grid. However, the approach requires significantly more computational effort.
Document ID
19950009438
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Slater, John W.
(NASA Lewis Research Center Cleveland, OH, United States)
Liou, Meng-Sing
(NASA Lewis Research Center Cleveland, OH, United States)
Hindman, Richard G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 94-0319
NASA-TM-106774
NAS 1.15:106774
E-9124-1
Report Number: AIAA PAPER 94-0319
Report Number: NASA-TM-106774
Report Number: NAS 1.15:106774
Report Number: E-9124-1
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Accession Number
95N15853
Funding Number(s)
CONTRACT_GRANT: NGT-50441
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Public Use Permitted.
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