Analysis estimation of pulse jet engine operation in detonation mode
- Authors: Seyfetdinov R.B.1, Seyfetdinov M.B.1, Gafurov S.A.1, Shakhmatov E.V.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 10, No 5 (2011)
- Pages: 221-226
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/2763
- DOI: https://doi.org/10.18287/2541-7533-2011-0-5(29)-221-226
- ID: 2763
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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 FederationM. B. Seyfetdinov
Samara State Aerospace University
Email: aeromach@mail.ru
Master of the Department of Power Plant Automatic Systems
Russian FederationS. A. Gafurov
Samara State Aerospace University
Email: sa.gafurov@gmail.com
Post-graduate Student of the Department of Power Plant Automatic Systems
Russian FederationE. 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