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Introduction and Formulation of the Problem

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

Abstract

Until recently the numerical and analytical investigations of the steady combustion of gas mixtures at supersonic speeds were carried out under the assumption of one-dimensional flow behind a normal shock wave or quasi-one-dimensional flow in a stream tube with given cross-section variations or with given variations of one flow parameter (for instance, at constant pressure).

Keywords

Shock Wave Steady Flow Supersonic Flow Stream Tube Normal Shock Wave 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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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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