The combustion and evaporation of liquid fuels at high pressures were investigated. Particular emphasis was placed on conditions where the liquid surface approaches the thermodynamic critical point during combustion. The influence of transient effects on a burning liquid fuel was also investigated through both analysis and measurements of the response of liquid monopropellant combustion to imposed pressure oscillations. Work was divided into four phases (1) Droplet combustion at high pressures, which consider both measurement and analysis of the porous sphere burning rate of liquids in a natural convection environment at elevated pressure. (2) High pressure droplet burning in combustion gases, which involved steady burning and evaporation o...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
The combustion characteristics of hydrazine strands were studied under both steady state and oscilla...
Experimental and theoretical results of critical pressure burning of fuel droplet
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Measurements were made of the burning rates and liquid surface temperatures for a number of alcohol ...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
The ultimate objective of this study is to obtain fundamental information relevant to combustion pro...
This is a joint research program, pursued by investigators at the University of Tokyo, UCSD, and NAS...
Combustion characteristics of liquid propellant droplets in air at near critical and super- critical...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
The combustion characteristics of hydrazine strands were studied under both steady state and oscilla...
Experimental and theoretical results of critical pressure burning of fuel droplet
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Measurements were made of the burning rates and liquid surface temperatures for a number of alcohol ...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
The ultimate objective of this study is to obtain fundamental information relevant to combustion pro...
This is a joint research program, pursued by investigators at the University of Tokyo, UCSD, and NAS...
Combustion characteristics of liquid propellant droplets in air at near critical and super- critical...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
The combustion characteristics of hydrazine strands were studied under both steady state and oscilla...
Experimental and theoretical results of critical pressure burning of fuel droplet