Email this article On the Numerical Simulation of Combustion in a Scramjet Combustor Using OpenFOAM
- Authors: Zhukov V.T.1, Novikova N.D.1, Feodoritova O.B.1
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Affiliations:
- Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
- Issue: Vol 11, No 2 (2019)
- Pages: 266-276
- Section: Article
- URL: https://journals.rcsi.science/2070-0482/article/view/203083
- DOI: https://doi.org/10.1134/S2070048219020170
- ID: 203083
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Abstract
In this paper, we present a methodology for the numerical simulation of the reacting flows of multicomponent fluid mixtures in a scramjet combustor based on solving the Navier-Stokes equation system. The combustion dynamics depending on the oxidizer’s oxidation ratio is studied, and the methodology of the numerical simulation on the multiprocessor supercomputer K-100 is developed using OpenFOAM.
About the authors
V. T. Zhukov
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Author for correspondence.
Email: zhukov@kiam.ru
Russian Federation, Moscow, 125047
N. D. Novikova
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Author for correspondence.
Email: nn@kiam.ru
Russian Federation, Moscow, 125047
O. B. Feodoritova
Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
Author for correspondence.
Email: feodor@kiam.ru
Russian Federation, Moscow, 125047
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