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Nonuniqueness of Solutions with Infinitely Thin Heat Release Fronts

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

Abstract

The statement made at the end of the previous section requires the assumption that beginning from some moment of the initial stage of motion (particularly from the first moment of motion) and permanently later the combustion proceeds in a detonation wave.

Keywords

Shock Wave Heat Release Detonation Wave Flame Front Adiabatic Shock 
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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