Volume 1, 2009Progress in Propulsion Physics
|Page(s)||185 - 204|
|Section||Liquid and Gelled Rocket Propulsion|
|Published online||16 September 2011|
Numerical simulation of operation processes in the combustion chamber and gas generator of oxygen-methane liquid rocket engine
The results of numerical simulations of processes in gas generators and combustion chambers operating on oxygen and methane are presented. Specific features of mixing, evaporation, and combustion of propellants have been investigated. The degree of combustion completeness in chambers with three types of injectors − coaxial-jet gas-liquid, liquid-liquid monopropellant, and bipropellant impinging-jets injectors − has been estimated.
© Owned by the authors, published by EDP Sciences, 2009