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JOURNALS // Preprints of the Keldysh Institute of Applied Mathematics // Archive

Keldysh Institute preprints, 2020 100, 12 pp. (Mi ipmp2891)

Comparative analysis of OpenFOAM solvers for the problem of supersonic flow around a cone at an angle of attack

A. E. Bondarev, A. E. Kuvshinnikov, T. N. Mikhailova, I. G. Ryzhova


Abstract: Three OpenFOAM solvers are selected to numerically solve the problem of supersonic flow around a cone. The angle of attack, the cone half-angle, and the Mach number changed. A number of test calculations were carried out. The fields of deviations of gas-dynamic quantities from the reference solution are analyzed for all solvers.

Keywords: comparative analysis of accuracy, compressible flow, supersonic flow, OpenFOAM.

DOI: 10.20948/prepr-2020-100



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