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A high resolution shock capturing scheme for high Mach number internal flowAn accurate shock capturing scheme is developed for high speed flow. The flux limited dissipation scheme can be converted to a symmetric TVD scheme in the case of a scalar conservation law. Application to an oblique shock wave problem shows the improved resolution and accuracy when compared to the results obtained by the adaptive dissipation method, while exhibiting comparable computational efficiency.
Document ID
19870007371
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yoon, Seokkwan
(Sverdrup Technology, Inc. Cleveland, OH, United States)
Jameson, Antony
(Princeton Univ. N. J., United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
E-3103
NAS 1.26:179523
NASA-CR-179523
Report Number: E-3103
Report Number: NAS 1.26:179523
Report Number: NASA-CR-179523
Accession Number
87N16804
Funding Number(s)
CONTRACT_GRANT: NAS3-24105
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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