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Keywords: RAE 2822 aerofoil
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Journal Articles
AN IMPLICIT FLUX‐DIFFERENCE SPLITTING METHOD FOR SOLVING THE EULER EQUATIONS ON ADAPTIVE TRIANGULAR GRIDS
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International Journal of Numerical Methods for Heat & Fluid Flow (1993) 3 (1): 63–77.
Published: 01 January 1993
..., an implicit treatment of the boundary conditions and the implementation of an adaptive grid strategy for global efficiency. The performance of the method is investigated for the GAMM test circular‐arc bump configuration and for the RAE 2822 aerofoil. © MCB UP Limited 1993 Transonic flows Roe flux...
