|
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.
Citation:
A. E. Bondarev, A. E. Kuvshinnikov, T. N. Mikhailova, I. G. Ryzhova, “Comparative analysis of OpenFOAM solvers for the problem of supersonic flow around a cone at an angle of attack”, Keldysh Institute preprints, 2020, 100, 12 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2891 https://www.mathnet.ru/eng/ipmp/y2020/p100
|
|