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A grid-independent approximate Riemann solver with applications to the Euler and Navier-Stokes equationsA new two-dimensional approximate Riemann solver has been developed that obtains fluxes on grid faces via wave decomposition. By utilizing information propagation in the velocity-difference directions rather than in the grid-normal directions, this flux function more appropriately interprets and hence more sharply resolves shock and shear waves when they lie oblique to the grid. The model uses five waves to describe the difference in states at a grid face. Two acoustic waves, one shear wave, and one entropy wave propagate in the direction defined by the local velocity difference vector, while the fifth wave is a shear wave that propagates at a right angle to the other four. Test cases presented include a shock reflecting off a wall, a pure shear wave, supersonic flow over an airfoil, and viscous separated airfoil flow. Results using the new model give significantly sharper shock and shear contours than a grid-aligned solver. Navier-Stokes computations over an aifoil show reduced pressure distortions in the separated region as a result of the grid-independent upwinding.
Document ID
19910034572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rumsey, Christopher L.
(NASA Langley Research Center Hampton, VA, United States)
Van Leer, Bram
(NASA Langley Research Center Hampton, VA, United States)
Roe, Philip L.
(Michigan, University Ann Arbor, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-0239
Accession Number
91A19195
Distribution Limits
Public
Copyright
Other

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