Add to ORKGA different approach to modeling of the thermochemistry of rocket engine combustion phenomena is presented. The methodology described is based on the hypothesis of a new variational principle applicable to compressible fluid mechanics. This hypothesis is extended to treat the thermochemical behavior of a reacting (equilibrium) gas in an open system
A detailed description of the equations and computer program for computations involving chemical equ...
Instabilities of motions in a combustion chamber are consequences of the coupled dynamics of combus...
Instabilities of motions in a combustion chamber are consequences of the coupled dynamics of combus...
A novel method for computing chemical equilibrium reactions in three-dimensional reacting fluid flow...
WOS:000354581800001International audienceCombustion in liquid rocket engines happens under severe th...
WOS:000354581800001International audienceCombustion in liquid rocket engines happens under severe th...
Models used to analyse scramjet engine cycles are typically either very simple or focused on specifi...
Nasa Lewis' studies of complex reacting systems at high temperature are discussed. The changes which...
Standard propulsive applications, such as liquid and hybrid rocket engines, are characterized by hig...
The combustion phenomena in liquid-propellant rocket engines are highly complex. The combustion occu...
CubeSats are small satelites who meet certain requirements of size, weight and other. These satelite...
This thesis compiles the process of upgrading two libraries (INIST and HGS) which provide to their u...
Chemical species and reactions of propellant systems determined for nonequilibrium flow - Performanc...
Combustion instability is a problem that has plagued the development of rocket-propelled devices sin...
An advanced engineering computational model has been developed to aid in the analysis of chemical ro...
A detailed description of the equations and computer program for computations involving chemical equ...
Instabilities of motions in a combustion chamber are consequences of the coupled dynamics of combus...
Instabilities of motions in a combustion chamber are consequences of the coupled dynamics of combus...
A novel method for computing chemical equilibrium reactions in three-dimensional reacting fluid flow...
WOS:000354581800001International audienceCombustion in liquid rocket engines happens under severe th...
WOS:000354581800001International audienceCombustion in liquid rocket engines happens under severe th...
Models used to analyse scramjet engine cycles are typically either very simple or focused on specifi...
Nasa Lewis' studies of complex reacting systems at high temperature are discussed. The changes which...
Standard propulsive applications, such as liquid and hybrid rocket engines, are characterized by hig...
The combustion phenomena in liquid-propellant rocket engines are highly complex. The combustion occu...
CubeSats are small satelites who meet certain requirements of size, weight and other. These satelite...
This thesis compiles the process of upgrading two libraries (INIST and HGS) which provide to their u...
Chemical species and reactions of propellant systems determined for nonequilibrium flow - Performanc...
Combustion instability is a problem that has plagued the development of rocket-propelled devices sin...
An advanced engineering computational model has been developed to aid in the analysis of chemical ro...
A detailed description of the equations and computer program for computations involving chemical equ...
Instabilities of motions in a combustion chamber are consequences of the coupled dynamics of combus...
Instabilities of motions in a combustion chamber are consequences of the coupled dynamics of combus...