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Computer simulation of some types of flows arising at interactions between a supersonic flow and a boundary layer

  • T. G. Elizarova
  • B. N. Chetverushkin
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 323)

Keywords

Supersonic Flow Oscillatory Regime Boltzmann Equa Keldysh Inst Boundary Layer Computer Simulation 
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References

  1. 1.
    Elizarova, T.G., Chetverushkin B.N. About a computing code for calculation of gasdynamic flows. JVM i MF, 1985, v.25, N 10, p.1526–1533.Google Scholar
  2. 2.
    Elizarova, T.G. On a class of kinetic-consistent difference schemes of gas dynamics. JVM i MP, 1987, v.27, N 11, p.1753–1757.Google Scholar
  3. 3.
    Antonov A.N., Elizarova T.G., Pavlov A.N., Chetverushkin B.N. Direct numerical simulation of oscillatory regimes in a flow about a spiked body. Preprint, Keldysh Inst. Appl. Math., USSR Ac. Sci., 1988, N 56.Google Scholar
  4. 4.
    Elizarova T.G., Chetverushin B.N., Sheretov Yu.V. On some results of calculation of a supersonic flow about an empty cylinder, carried out with kinetic-consistent difference schemes. Preprint, Keldysh Inst. Appl. Math., USSR Ac. Sci., 1988, N 97.Google Scholar
  5. 5.
    Graur I.A., Elizarova, T.G., Chetverushkin B.N. On application of kinetic-consistent difference schemes for calculating heat exchange in supersonic gasdynamic flows. Preprint, Keldysh Inst. *** DIRECT SUPPORT *** A3418252 00010Google Scholar

Copyright information

© Springer-Verlag 1989

Authors and Affiliations

  • T. G. Elizarova
    • 1
  • B. N. Chetverushkin
    • 1
  1. 1.M.V. Keldysh Institute of Applied MathematicsAcademy of Sciences of the USSRMoscow

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