The objective is to study the evaporation and combustion of LOX under supercritical and subcritical conditions both experimentally and theoretically. In the evaporation studies, evaporation rate and surface temperature were measured when LOX vaporizing in helium environments at pressures ranging from 5 to 68 atm. A Varian 3700 gas chromatograph was employed to measure the oxygen concentration above the LOX surface. For the combustion tests, high-magnification video photography was used to record direct images of the flame shape of a LOX/H2/He laminar diffusion flame. The gas composition in the post-flame region is also being measured with the gas sampling and chromatography analysis. These data are being used to validate the theoretical mod...
This article deals with the application of OH planar laser-induced fluorescence (PLIF) to the study ...
Methane and Liquefied Natural Gas (LNG) have been recently considered as propellants, together with ...
This paper presents an investigation of LOX/CH4 Liquid Rocket Engines injector flames to investigate...
The objective was to achieve a better understanding of the combustion processes of liquid oxygen and...
Modern liquid rocket engines often use liquid oxygen (LOX) and liquid hydrogen (LH2) as propellants ...
High-pressure combustion devices, such as liquid rocket engines, are usually characterized by transc...
An experimental program using liquid oxygen (LOX) and RP-1 as the propellants and supercritical LOX ...
International audienceAbstract: Planar laser induced fluorescence (PLIF) of OH is used to examine fl...
This work presents a study of non-premixed flames at supercritical-pressure conditions. Emphasis is ...
The aim of the present work is the investigation of the combustion phenomenon in liquid-propellant r...
The increasing interest in reusable LOx/CH4 first-stage liquid rocket engines requires the further d...
The supercritical conditions are typically encountered in the high-pressure combustion devices such ...
Thesis (Master's)--University of Washington, 2021To develop more effective and better cryogenic powe...
A detailed understanding of liquid propellant combustion is necessary for the development of improve...
The primary goal of this study is to numerically model the transcritical mixing and reacting flow pr...
This article deals with the application of OH planar laser-induced fluorescence (PLIF) to the study ...
Methane and Liquefied Natural Gas (LNG) have been recently considered as propellants, together with ...
This paper presents an investigation of LOX/CH4 Liquid Rocket Engines injector flames to investigate...
The objective was to achieve a better understanding of the combustion processes of liquid oxygen and...
Modern liquid rocket engines often use liquid oxygen (LOX) and liquid hydrogen (LH2) as propellants ...
High-pressure combustion devices, such as liquid rocket engines, are usually characterized by transc...
An experimental program using liquid oxygen (LOX) and RP-1 as the propellants and supercritical LOX ...
International audienceAbstract: Planar laser induced fluorescence (PLIF) of OH is used to examine fl...
This work presents a study of non-premixed flames at supercritical-pressure conditions. Emphasis is ...
The aim of the present work is the investigation of the combustion phenomenon in liquid-propellant r...
The increasing interest in reusable LOx/CH4 first-stage liquid rocket engines requires the further d...
The supercritical conditions are typically encountered in the high-pressure combustion devices such ...
Thesis (Master's)--University of Washington, 2021To develop more effective and better cryogenic powe...
A detailed understanding of liquid propellant combustion is necessary for the development of improve...
The primary goal of this study is to numerically model the transcritical mixing and reacting flow pr...
This article deals with the application of OH planar laser-induced fluorescence (PLIF) to the study ...
Methane and Liquefied Natural Gas (LNG) have been recently considered as propellants, together with ...
This paper presents an investigation of LOX/CH4 Liquid Rocket Engines injector flames to investigate...