Application of Finite Difference TVD Methods in Hypersonic Aerodynamics

  • Yury DimitrienkoEmail author
  • Mikhail Koryakov
  • Andrey Zakharov
Conference paper
Part of the Lecture Notes in Computer Science book series (LNCS, volume 9045)


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.


Computational fluid dynamics Hypersonic flows TVD schemes Parallel processing 



The reported study was supported by the Supercomputing Center of Lomonosov Moscow State University.


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Copyright information

© Springer International Publishing Switzerland 2015

Authors and Affiliations

  • Yury Dimitrienko
    • 1
    Email author
  • Mikhail Koryakov
    • 1
  • Andrey Zakharov
    • 1
  1. 1.Bauman Moscow State Technical UniversityRussiaMoscow

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