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The Accuracy of Shock Capturing in Two Spatial DimensionsAn assessment of the accuracy of shock capturing schemes is made for two-dimensional steady flow around a cylindrical projectile. Both a linear fourth-order method and a nonlinear third-order method are used in this study. It is shown, contrary to conventional wisdom, that captured two-dimensional shocks are asymptotically first-order, regardless of the design accuracy of the numerical method. The practical implications of this finding are discussed in the context of the efficacy of high-order numerical methods for discontinuous flows.
Document ID
19970022177
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Carpenter, Mark H.
(NASA Langley Research Center Hampton, VA United States)
Casper, Jay H.
(Old Dominion Univ. Norfolk, VA United States)
Date Acquired
August 17, 2013
Publication Date
June 1, 1997
Publication Information
Publication: An Investigation of High-Order Shock-Capturing Methods for Computational Aeroacoustics
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 97-2107
Meeting Information
Meeting: Computational Fluid Dynamics
Location: Snowmass, CO
Country: United States
Start Date: June 29, 1997
End Date: July 2, 1997
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
97N22774
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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