Add to ORKGCombustion instability, where unsteady heat release couples with acoustic modes, has long been an area of concern in liquid rocket engines. Accurate modeling of the acoustic normal modes of the combustion chamber is important to understanding and preventing combustion instability. The injector resistance can have a significant influence on the chamber normal mode shape, and hence on the system stability
The theory and procedures for determining the characteristics of pressure oscillations in rocket eng...
Analytical studies have been made of the relative combustion stability of various propellant combina...
Combustion devices are prone to combustion instabilities. They arise from a constructive coupling be...
Combustion instability, where unsteady heat release couples with acoustic modes, has long been an ar...
Combustion instability in solid rocket motors and liquid engines has long been a subject of concern....
High frequency combustion instability has recently been observed by Rocketdyne in a 40K thrust metha...
This thesis focuses on the understanding and the prediction of combustion instability in high-pressu...
Combustion instabilities are strong acoustic disturbances that often form spontaneously inside rocke...
This article explores the possibility of analyzing combustion instabilities in liq- uid rocket engin...
This paper reports the investigation of acoustic combustion instability experienced during repetitiv...
This paper is a compilation of the research efforts of five different groups (Bertin Technologies an...
Small amplitude linear analysis of combustion instability with finite Mach number flow and acoustic ...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
It is well known that under some operating conditions, rocket engines (using solid or liquid fuels) ...
High frequency combustion instability, the most destructive kind, is generally solved on a per engin...
The theory and procedures for determining the characteristics of pressure oscillations in rocket eng...
Analytical studies have been made of the relative combustion stability of various propellant combina...
Combustion devices are prone to combustion instabilities. They arise from a constructive coupling be...
Combustion instability, where unsteady heat release couples with acoustic modes, has long been an ar...
Combustion instability in solid rocket motors and liquid engines has long been a subject of concern....
High frequency combustion instability has recently been observed by Rocketdyne in a 40K thrust metha...
This thesis focuses on the understanding and the prediction of combustion instability in high-pressu...
Combustion instabilities are strong acoustic disturbances that often form spontaneously inside rocke...
This article explores the possibility of analyzing combustion instabilities in liq- uid rocket engin...
This paper reports the investigation of acoustic combustion instability experienced during repetitiv...
This paper is a compilation of the research efforts of five different groups (Bertin Technologies an...
Small amplitude linear analysis of combustion instability with finite Mach number flow and acoustic ...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
It is well known that under some operating conditions, rocket engines (using solid or liquid fuels) ...
High frequency combustion instability, the most destructive kind, is generally solved on a per engin...
The theory and procedures for determining the characteristics of pressure oscillations in rocket eng...
Analytical studies have been made of the relative combustion stability of various propellant combina...
Combustion devices are prone to combustion instabilities. They arise from a constructive coupling be...