Models of Non-Stationary Thermodynamic Processes in Rocket Engines Taking into Account a Chemical Equilibrium of Combustion Products

Models of Non-Stationary Thermodynamic Processes in Rocket Engines Taking into Account a Chemical Equilibrium of Combustion Products

<p>The paper considers the two approach-based techniques for calculating the non-stationary intra-chamber processes in solid-propellant rocket engine (SPRE). The first approach assumes that the combustion products are a mechanical mix while the other one supposes it to be the mix, which is in...

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Bibliographic Details
Main Authors: A. V. Aliev, O. A. Voevodina, E. S. Pushina
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2015-01-01
Series:Nauka i Obrazovanie
Subjects:
rocket engine
propellant
chemical equilibrium
internal ballistics
QR method
genetic algorithm
Online Access:http://technomag.edu.ru/jour/article/view/118

Internet

http://technomag.edu.ru/jour/article/view/118

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