Comparative analysis of OpenFOAM solvers for the problem of supersonic flow around a cone at an angle of attack
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
Publication language:russian, pages:12
Research direction:
Mathematical modelling in actual problems of science and technics
