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Computational efficiency achieved by time splitting of finite difference operators.A technique is presented for computing multidimensional time-dependent flow fields that avoids much of the inefficiency typically found in finite difference calculations. The technique initially divides the flow field into regions, each containing a mesh of general quadrilateral cells chosen to provide spatial resolution of the local features of the flow. A finite difference operator of second order accuracy, consisting of a sequence of one-dimensional operators (each operating at near maximum Courant-Friedrich-Lewy number) is then constructed for each region. Numerical results illustrating the technique for inviscid flows about simple bodies that generate shock waves, embedded shock waves, and expansion fans are presented and compared with exact theory.
Document ID
19720033284
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maccormack, R. W.
(NASA Ames Research Center Computational Fluid Dynamics Branch, Moffett Field, Calif., United States)
Paullay, A. J.
(Bronx Community College Bronx, N.Y., United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 72-154
Report Number: AIAA PAPER 72-154
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: San Diego, CA
Start Date: January 17, 1972
End Date: January 19, 1972
Sponsors: Science Research Council
Accession Number
72A16950
Distribution Limits
Public
Copyright
Other

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