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The space-time solution element method: A new numerical approach for the Navier-Stokes equationsThis paper is one of a series of papers describing the development of a new numerical method for the Navier-Stokes equations. Unlike conventional numerical methods, the current method concentrates on the discrete simulation of both the integral and differential forms of the Navier-Stokes equations. Conservation of mass, momentum, and energy in space-time is explicitly provided for through a rigorous enforcement of both the integral and differential forms of the governing conservation laws. Using local polynomial expansions to represent the discrete primitive variables on each cell, fluxes at cell interfaces are evaluated and balanced using exact functional expressions. No interpolation or flux limiters are required. Because of the generality of the current method, it applies equally to the steady and unsteady Navier-Stokes equations. In this paper, we generalize and extend the authors' 2-D, steady state implicit scheme. A general closure methodology is presented so that all terms up through a given order in the local expansions may be retained. The scheme is also extended to nonorthogonal Cartesian grids. Numerous flow fields are computed and results are compared with known solutions. The high accuracy of the scheme is demonstrated through its ability to accurately resolve developing boundary layers on coarse grids. Finally, we discuss applications of the current method to the unsteady Navier-Stokes equations.
Document ID
19950011621
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Scott, James R.
(NASA Lewis Research Center Cleveland, OH, United States)
Chang, Sin-Chung
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-106818
E-9357
NAS 1.15:106818
AIAA PAPER 95-0763
Report Number: NASA-TM-106818
Report Number: E-9357
Report Number: NAS 1.15:106818
Report Number: AIAA PAPER 95-0763
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 9, 1995
End Date: January 12, 1995
Accession Number
95N18036
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Public Use Permitted.
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