Analysis estimation of pulse jet engine operation in detonation mode

Cover Page

Cite item

Full Text

Abstract

The problem of deflagration-to-detonation transition in pulse jet engines is described in this work. The conditions of deflagration-to-detonation transition have been considered for hydrocarbon fuel. The disadvantages of technologies of predetonator and shock implosion are discussed.

About the authors

R. B. Seyfetdinov

Samara State Aerospace University

Author for correspondence.
Email: fagott@bk.ru

Candidate of Technical Sciences

Russian Federation

M. B. Seyfetdinov

Samara State Aerospace University

Email: aeromach@mail.ru

Master of the Department of Power Plant Automatic Systems

Russian Federation

S. A. Gafurov

Samara State Aerospace University

Email: sa.gafurov@gmail.com

Post-graduate Student of the Department of Power Plant Automatic Systems

Russian Federation

E. V. Shakhmatov

Samara State Aerospace University

Email: shakhm@ssau.ru

Doctor of Technical Sciences, Professor

Rector, Head of the Department of Power Plant Automatic Systems

Russian Federation

References

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies