Computation of the Supersonic Flow Region

  • Gorimir G. Cherny
Part of the International Centre for Mechanical Sciences book series (CISM, volume 36)


For numerical computations of two-dimensional steady supersonic flows past bodies the method of characteristics is widely used. In the papers dealing with flows with combustion, different variants of calculations have been suggested with transition from one strip to another and with drawing the characteristics in backward direction.


Shock Wave Steady Flow Detonation Wave Node Point Supersonic Flow 
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Copyright information

© Springer-Verlag Wien 1973

Authors and Affiliations

  • Gorimir G. Cherny
    • 1
  1. 1.University of MoscowRussia

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