Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environment. The experimental range of these tests involved gas temperatures of 1660-2530 K, oxygen concentrations of 0-42% by mass and droplet diameters (employing both droplets and porous spheres) of 0.11-1.91 cm. at atmospheric pressure. A simplified hybrid combustion theory was developed which was found to correlate the present results as well as the experimental measurements of other investigators. Measurements were also made of the monopropellant strand burning rates and liquid surface temperatures of a number of nitrate ester fuels and hydrazine at elevated pressures. The temperature measurements for the nitrate esters were found to be in goo...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
The combustion and evaporation of liquid fuels at high pressures were investigated. Particular empha...
Measurements were made of the burning rates and liquid surface temperatures for a number of alcohol ...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
The combustion characteristics of hydrazine strands were studied under both steady state and oscilla...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
Combustion characteristics of liquid propellant droplets in air at near critical and super- critical...
Hybrid and decomposition combustion of hydrazine fuels using flat flame burner to provide high tempe...
Experimental and theoretical results of critical pressure burning of fuel droplet
The ultimate objective of this study is to obtain fundamental information relevant to combustion pro...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
The combustion and evaporation of liquid fuels at high pressures were investigated. Particular empha...
Measurements were made of the burning rates and liquid surface temperatures for a number of alcohol ...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
The combustion characteristics of hydrazine strands were studied under both steady state and oscilla...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
Combustion characteristics of liquid propellant droplets in air at near critical and super- critical...
Hybrid and decomposition combustion of hydrazine fuels using flat flame burner to provide high tempe...
Experimental and theoretical results of critical pressure burning of fuel droplet
The ultimate objective of this study is to obtain fundamental information relevant to combustion pro...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...