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Computation of Subsonic Flow Region

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

Abstract

For numerical solutions of problems on steady supersonic flow around blunt-nosed bodies in USSR the method suggested by G.F. Telenin [6] and usually called the method of straight lines is widely used. In a series of papers [7–12] this method has been developed for application to combustible gas mixture flows. For the model of infinitely thin detonation wave the method of straight lines applies completely analogous to adiabatic gas flows, the only difference being that in the energy conservation law across the shock the heat release term Q appears.

Keywords

Shock Wave Steady Flow Detonation Wave Node Point Combustion Front 
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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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