This article explores the possibility of analyzing combustion instabilities in liquid rocket
engines by making use of Large Eddy Simulations (LES). Calculations are carried out for a …

Combustion instability is investigated in a model chamber by changing the recess length of
a gas-centered swirl coaxial injector ranging from 0 mm to 20 mm with a 4 mm interval …

The flame transfer function (FTF) and acoustic transfer function (ATF) are estimated
experimentally and numerically, respectively, and both are combined to predict combustion …

Mixing and combustion characteristics of swirl coaxial jet injector for gas–liquid injection are
investigated numerically with a model of gas–gas injection. The gas–liquid injector, widely …

Fuel combinations with substantial differences in reactivity, such as diesel/CNG, represent
one of the most promising alternative combustion strategies these days. In general, the …

This study investigates the effects of injector spacing and momentum flux ratio on
combustion instability in a model chamber with single and two injectors, both experimentally …

THERE are two conflicting concerns in the development of new rocket engine combustors,
which include performance and stability. Generally, combustors of high performance have …

Thermo-acoustic instability of methane/air flames in an industrial gas-turbine combustor is
numerically investigated adopting CFD analysis. The combustor has 37 EV burners through …

This work provides an assessment of an experimental method for characterizing combustion
stability of liquid rocket injectors. The research has shown that the single-element laboratory …

This paper presents the state of the art and challenges in the design of rocket motor case
structures RMCS it briefly describes the construction of RMCS then lists the different …