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Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAn implicit finite-difference procedure for unsteady three-dimensional flow capable of handling arbitrary geometry through the use of general coordinate transformations is described. Viscous effects are optionally incorporated with a "thin-layer" approximation of the Navier-Stokes equations. An implicit approximate factorization technique is employed so that the small grid sizes required for spatial accuracy and viscous resolution do not impose stringent stability limitations. Results obtained from the program include transonic inviscid or viscous solutions about simple body configurations. Comparisons with existing theories and experiments are made. Numerical accuracy and the effect of three-dimensional coordinate singularities are also discussed.
Document ID
19990027655
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Pulliam, Thomas H.
(NASA Ames Research Center Moffett Field, CA United States)
Steger, Joseph L.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 19, 2013
Publication Date
February 1, 1980
Publication Information
Publication: AIAA Journal
Publisher: American Institute of Aeronautics and Astronautics
Volume: 18
Issue: 2
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA Paper 78-10R
Report Number: AIAA Paper 78-10R
Meeting Information
Meeting: Aerospace Sciences
Location: Huntsville, AL
Country: United States
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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