An analytical model based on linearized Euler equations (LEE) is developed and used in conjunction with a validating experiment to study combustion instability. The LEE model features mean flow effects, entropy waves, adaptability for more physically-realistic boundary conditions, and is generalized for multiple-domain conditions. The model calculates spatial modes, resonant frequencies and linear growth rates of the overall system. The predicted resonant frequencies and spatially-resolved mode shapes agree with the experimental data from a longitudinally-unstable model rocket combustor to within 7%. Different gaseous fuels (methane, ethylene, and hydrogen) were tested under fixed geometry. Tests with hydrogen were stable, whereas ethylene,...
International audienceUnderstanding the flame dynamics in combustion chambers is still an important ...
Throughout the study of high frequency combustion instability in a single element Continuously Varia...
International audienceHigh-frequency instabilities in liquid propellant rocket engines are experimen...
An experimental investigation of high-frequency longitudinal combustion instability using a continuo...
The combustion process within a single element dump combustor was studied using the Continuously Var...
Several test cases in the literature have shown that both transverse and longitudinal high frequency...
The utility of high fidelity (HF) pressure measurements from Continuous Variable Resonance Combustor...
Throughout the study of high frequency combustion instability in a single element Continuously Varia...
Experimental data from a longitudinally unstable uni-element model rocket combustor are analyzed usi...
The development of a velocity-based mechanistic combustion response model and its application to liq...
The overall objective of the current research is to evaluate if and how computational fluid dynamics...
Gaseous methane and 90% hydrogen peroxide at an equivalence ratio of 0.8 were used to study combusti...
High frequency combustion instabilities in liquid propellant rocket engines are spontaneously occurr...
Nonlinear Euler simulations were conducted for two different geometries in order to characterize the...
Longitudinal high frequency combustion instability is the focus of the present work with particular ...
International audienceUnderstanding the flame dynamics in combustion chambers is still an important ...
Throughout the study of high frequency combustion instability in a single element Continuously Varia...
International audienceHigh-frequency instabilities in liquid propellant rocket engines are experimen...
An experimental investigation of high-frequency longitudinal combustion instability using a continuo...
The combustion process within a single element dump combustor was studied using the Continuously Var...
Several test cases in the literature have shown that both transverse and longitudinal high frequency...
The utility of high fidelity (HF) pressure measurements from Continuous Variable Resonance Combustor...
Throughout the study of high frequency combustion instability in a single element Continuously Varia...
Experimental data from a longitudinally unstable uni-element model rocket combustor are analyzed usi...
The development of a velocity-based mechanistic combustion response model and its application to liq...
The overall objective of the current research is to evaluate if and how computational fluid dynamics...
Gaseous methane and 90% hydrogen peroxide at an equivalence ratio of 0.8 were used to study combusti...
High frequency combustion instabilities in liquid propellant rocket engines are spontaneously occurr...
Nonlinear Euler simulations were conducted for two different geometries in order to characterize the...
Longitudinal high frequency combustion instability is the focus of the present work with particular ...
International audienceUnderstanding the flame dynamics in combustion chambers is still an important ...
Throughout the study of high frequency combustion instability in a single element Continuously Varia...
International audienceHigh-frequency instabilities in liquid propellant rocket engines are experimen...