Numerical Estimation Method for the NonStationary Thrust of Pulsejet Ejector Nozzle

Numerical Estimation Method for the NonStationary Thrust of Pulsejet Ejector Nozzle

<p>The article considers a calculation method for the non-stationary thrust of pulsejet ejector nozzle that is based on detonation combustion of gaseous fuel.</p><p>To determine initial distributions of the thermodynamic parameters inside the detonation tube was carried out a rapid...

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Bibliographic Details
Main Authors: A. Yu. Mikushkin, A. A. Samoilova, G. Y. Bivol, A. E. Korobov, S. V. Golovastov
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2016-01-01
Series:Nauka i Obrazovanie
Subjects:
ejector
detonation
chemical equilibrium
air consumption
Online Access:http://technomag.edu.ru/jour/article/view/35

Internet

http://technomag.edu.ru/jour/article/view/35

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