Abstract
The numerical method for solving of the hypersonic nonequilibrium aerogasdynamics problems is suggested. The method is based on the full three-dimensional Navier-Stokes equations, supplemented by the equations of chemical kinetics and the finite difference TVD method. The developed algorithms are implemented in the computer-aided software package SIGMA. The results of simulation of the hypersonic flow about the spherical nose segment of a model hypersonic vehicle are presented.
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Acknowledgements
The reported study was supported by the Supercomputing Center of Lomonosov Moscow State University.
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Dimitrienko, Y., Koryakov, M., Zakharov, A. (2015). Application of Finite Difference TVD Methods in Hypersonic Aerodynamics. In: Dimov, I., Faragó, I., Vulkov, L. (eds) Finite Difference Methods,Theory and Applications. FDM 2014. Lecture Notes in Computer Science(), vol 9045. Springer, Cham. https://doi.org/10.1007/978-3-319-20239-6_15
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DOI: https://doi.org/10.1007/978-3-319-20239-6_15
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