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Higher order accuracy for upwind methods by using the compatibility equationsA new algorithm has been developed for obtaining higher order accuracy in upwind schemes for the Euler and Navier-Stokes equations. In this method, the compatibility relations for the Euler equations are used to construct formulas for the higher order interpolates. Using these formulas, computed results are obtained for steady, inviscid flow through a nozzle and also steady, inviscid and viscous flow over an airfoil. These results are compared with results obtained by using a minmod limiter function. The comparisons show improved accuracy throughout the flow field with the use of the compatibility equations.
Document ID
19910056095
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goorjian, Peter M.
(NASA Ames Research Center Moffett Field, CA, United States)
Obayashi, Shigeru
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-1543
Report Number: AIAA PAPER 91-1543
Meeting Information
Meeting: AIAA Computational Fluid Dynamics Conference
Location: Honolulu, HI
Country: United States
Start Date: June 24, 1991
End Date: June 27, 1991
Accession Number
91A40718
Distribution Limits
Public
Copyright
Other

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