Geodesic
On a computational technique for simulation of scramjet combustor by means of OpenFOAM
Matematičeskoe modelirovanie, Tome 30 (2018) no. 8, pp. 32-50.

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A methodology for numerical simulation of flows in the scramjet combustor provides. The approach is based on the numerical solution of the Navier–Stokes system of the reacting flows of multicomponent fluid mixtures. The dynamics of combustion processes is studied depending on the coefficient of oxidizer excess and the technology is developed for numerical simulations on a multiprocessor supercomputer K-100 by means of OpenFOAM.
Keywords: numerical simulation, multicomponent flows, scramjet combustor, OpenFOAM. 
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V. T. Zhukov; N. D. Novikova; O. B. Feodoritova. On a computational technique for simulation of scramjet combustor by means of OpenFOAM. Matematičeskoe modelirovanie, Tome 30 (2018) no. 8, pp. 32-50. http://geodesic.mathdoc.fr/item/MM_2018_30_8_a2/

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