Experimental study of detonation initiation and behaviour of combustion chamber model for the pulse-jet detonating engine

Аuthors

Frolov V. N.^*, Garanin I. V.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: 28474@mail.ru
**e-mail: garanin-nio203@yandex.ru

Abstract

A systems of detonation initiation are studied in the combustion chamber. The parameters of the combustion chamber are rated in the self-oscillation mode, the maximum frequency of pulsations is set.

Keywords:

detonation engine, detonation, combustion chamber

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